Table of Contents
Active Control and Closed-Loop Identification of Flutter Instability in a Typical Section Airfoil
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
Active Vibration Control of Composite Spacecraft Booms Exposed To Solar Radiant Heating
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
Energy-Frequency-Time Analysis of Structural Vibrations Using Hilbert-Huang Transform
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
Structural Control Using Inverse H2 Optimal Theory
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
Neural Network-Based Frequency-Domain Vibration Modeling for Black Hawk Helicopter
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
A Model for Polar Shells with Thickness Extension
ASC-9: Adaptive Structure Control and Modeling • Thursday, 22 April 2004 • 0930 hrs
Powder Processing and Characterization of Hydrogen Embrittlement Resistant NASA-23 Alloy
SDM-56: Advanced Propulsion Materials • Thursday, 22 April 2004 • 0930 hrs
Friction Stir Welding of GR-Cop 84 for Combustion Chamber Liners
SDM-56: Advanced Propulsion Materials • Thursday, 22 April 2004 • 0930 hrs
Nanocomposite Rocket Ablative Materials: Processing, Microstructure, and Performance
SDM-56: Advanced Propulsion Materials • Thursday, 22 April 2004 • 0930 hrs
Ceramic Matrix Composites Cooled Panel Development for Advanced Propulsion Systems
SDM-56: Advanced Propulsion Materials • Thursday, 22 April 2004 • 0930 hrs
Fatigue Failure Predictions at Stress Concentrations Using Critical Distance Methods
SDM-56: Advanced Propulsion Materials • Thursday, 22 April 2004 • 0930 hrs
Artificial Neural Network for Multiple Aeroelastic Analysis
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
AE/ASE Simulation of Aerospace Vehicles Using STARS Software
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
Single/Double Hopf Bifurcation and Aeroelastic Instability of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
Static and Dynamic Aeroelastic Analysis of Structural Wing Fold Hinges that are Employed as an Aeroelastic Tailoring Tool
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
Analytical Aeroelastic Characteristics of F-16 Asymmetric External Store Configurations
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
Linear/Nonlinear Aeroelastic Computation of 2-D Lifting Surfaces Using a Combined CFD/Analytical Approach
SDM-30: Aeroelastic Analysis • Tuesday, 20 April 2004 • 1400 hrs
Variable Stiffness Spar Wind-Tunnel Model Development and Testing
SDM-11: Aeroelastic Applications • Monday, 19 April 2004 • 1430 hrs
Hypersonic Aerothermoelastic Studies for Reusable Launch Vehicles
SDM-11: Aeroelastic Applications • Monday, 19 April 2004 • 1430 hrs
Effects of Internal Friction on the Dynamic Behavior of Aeroelastic Systems
SDM-11: Aeroelastic Applications • Monday, 19 April 2004 • 1430 hrs
Aeroservoelastic Gust Response Analysis for the Design of Transport Aircrafts
SDM-11: Aeroelastic Applications • Monday, 19 April 2004 • 1430 hrs
Trajectory Optimization Strategies for Supercavitating Underwater Vehicles
SDM-11: Aeroelastic Applications • Monday, 19 April 2004 • 1430 hrs
An Overset Field-Panel Method for Unsteady Transonic Aerodynamic Influence Coefficient Matrix Generation
SDM-1: Aeroelastic Modeling Methods • Monday, 19 April 2004 • 0930 hrs
An Approach to Induced Drag Reduction and its Experimental Evaluation
SDM-1: Aeroelastic Modeling Methods • Monday, 19 April 2004 • 0930 hrs
CFD-Based Aeroelastic Response of an Active Aeroelastic Wing
SDM-1: Aeroelastic Modeling Methods • Monday, 19 April 2004 • 0930 hrs
Identifying Parameter-Dependent Volterra Kernels to Predict Aeroelastic Instabilities
SDM-1: Aeroelastic Modeling Methods • Monday, 19 April 2004 • 0930 hrs
Design of Low-boom Supersonic Business Jet with Evolutionary Algorithms Using Adaptive Unstructured Mesh
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
Unsteady Aerodynamic Shape Sensitivities for Airplane Aeroservoelastic Configuration Optimization
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
Joined-Wing Sensor-Craft Configuration Design
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
Optimum Design Framework for Integrally Twisted Helicopter Blades
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
State-Space Unsteady Aerodynamics for Aeroservoelastic Configuration Shape Optimization of Flight Vehicles
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
Multilevel Variable Fidelity Optimization of a Morphing Unmanned Aerial Vehicle
SDM-31: Aeroelastic Optimization • Tuesday, 20 April 2004 • 1400 hrs
Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
Flight Testing a Micro Air Vehicle Using Morphing for Aeroservoelastic Control
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
Modeling of Aeroservoelastic Systems with Structural and Aerodynamic Variations
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
High Resolution Turbulence Treatment of F/A-18 Tail Buffet
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
Assessing Videogrammetry for Static Aeroelastic Testing of a Wind-Tunnel Model
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
Low Speed Wind Tunnel Buffet Testing on the F/A-22
SDM-22: Aeroservoelasticity and Aeroelastic Testing • Tuesday, 20 April 2004 • 0930 hrs
Development of a Deployable Boom for Microsatellites Using Elastic Memory Composite Material
GSF-9: Analysis and Testing of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Analytical and Experimental Characterization of Gravity Induced Deformations in Subscale Gossamer Structures
GSF-9: Analysis and Testing of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Carbon Fibre Reinforced Plastic Tape Springs
GSF-9: Analysis and Testing of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Modeling of Snap-Back Bending Response of Doubly Slit Cylindrical Shells
GSF-9: Analysis and Testing of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
An Exact Dynamic Stiffness Matrix for a Two-part Beam-mass System and Its Applications
SDM-2: Beams, Plates and Shells I • Monday, 19 April 2004 • 0930 hrs
The Vlasov Theory of the Variational Asymptotic Beam Sectional Analysis
SDM-2: Beams, Plates and Shells I • Monday, 19 April 2004 • 0930 hrs
Flap-Torsion Coupling in Prismatic-Sections
SDM-2: Beams, Plates and Shells I • Monday, 19 April 2004 • 0930 hrs
The Brazier effect in multi-bay aerofoil sections
SDM-2: Beams, Plates and Shells I • Monday, 19 April 2004 • 0930 hrs
Analytical Modeling of Twist Actuators for Pretwisted Anisotropic Strips
SDM-2: Beams, Plates and Shells I • Monday, 19 April 2004 • 0930 hrs
Shape and Layup Optimization of Laminated Composite Shells Based on Integrated Framework of Modeling and Analysis
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Strategies for Tailoring Wings with Bend-Twist Coupling: Part Two
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Analysis of Stainless Steel Sandwich Panels with a Metal Foam Core for Lightweight Fan Blade Design
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Structural Optimization of Composite Rotor Blades
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Closed-Form Non-Linear Sectional Analysis in the Presence of Delamination
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Pressurization of CF/Epoxy Model Tank at LN2 Temperature and Identification of Leak Path Formation in Tank Wall
SDM-38: Beams, Plates and Shells II • Wednesday, 21 April 2004 • 0930 hrs
Finite Element Analysis in Concurrent Processing: Computational Issues
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Hierarchical Strategy for Rapid Finite Element Analysis
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Adaptive Quadrilateral Refinement Considering Multiple Quantities of Interest
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
First-order Shear Deformable Subdivision Element Consistent with Loop-Subdivision Surfaces
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Radial Basis Meshless Local Petrov-Galerkin Method for Thick Beams
- I Raju and
- D Phillips
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Analysis of a Column Subjected to Follower Forces by a Meshless Local Petrov-Galerkin Method
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Thermo-Elastic Triangular Sandwich Element for the Complete Stress Field Based on a Single-Layer Theory
SDM-32: Computational Structural Mechanics I • Tuesday, 20 April 2004 • 1400 hrs
Application of the Discontinuous Solid-Like Shell Element to Delamination
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
High-order Finite Elements Reduced Models for Use in a Flutter Design Tool
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
Construction of Reduced System by Two-Level Condensation Scheme and Refined Sensitivity Analysis
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
Finite Element Load Updating for Plates
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
Finite Element Model Updating Using Response Surface Method
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
A Finite Element Analysis Based on Higher-order Zig-zag Shell Theory for Laminated Composites with Multiple Delaminations
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
Investigation of Instability in Crash Analysis on Various Computing Environments
SDM-57: Computational Structural Mechanics II • Thursday, 22 April 2004 • 0930 hrs
Actuation of Kagome Lattice Structures
SDM-3: Concepts for Morphing and Reconfigurable Structures • Monday, 19 April 2004 • 0930 hrs
Bi-stable Concepts for Reconfigurable Structures
SDM-3: Concepts for Morphing and Reconfigurable Structures • Monday, 19 April 2004 • 0930 hrs
An Asymmetrically-Bistable Monolithic Energy-Storing Structure
SDM-3: Concepts for Morphing and Reconfigurable Structures • Monday, 19 April 2004 • 0930 hrs
A Novel Actuated Composite Tape-Spring for Deployable Structures
SDM-3: Concepts for Morphing and Reconfigurable Structures • Monday, 19 April 2004 • 0930 hrs
Multi-configuration Space Frames
SDM-3: Concepts for Morphing and Reconfigurable Structures • Monday, 19 April 2004 • 0930 hrs
A Spider Technology Overview
GSF-10: Control of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Demonstration of Dynamic Tailoring for Gossamer Structures
GSF-10: Control of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Boundary Actuation Shape Control Strategies for Thin Film Single Surface Shells
GSF-10: Control of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Parametric Uncertainty Quantification of an Inflatable/Rigidizable Hexapod
GSF-10: Control of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
Active Control of Inflatable Structure Membrane Wrinkles Using Genetic Algorithm and Neural Network
GSF-10: Control of Gossamer Spacecraft • Wednesday, 21 April 2004 • 0930 hrs
The Dual Role of Cohesive Layer Model in Delamination Investigation
SDM-12: Damage Detection and Evaluation I • Monday, 19 April 2004 • 1430 hrs
Progressive Failure of Composite Laminates Using LaRC02 Criteria
SDM-12: Damage Detection and Evaluation I • Monday, 19 April 2004 • 1430 hrs
Towards Hierarchical Modeling of Damage in Composite Structures
SDM-12: Damage Detection and Evaluation I • Monday, 19 April 2004 • 1430 hrs
Development of a Fatigue Crack Growth Coupon for Highly Plastic Stress Conditions
SDM-12: Damage Detection and Evaluation I • Monday, 19 April 2004 • 1430 hrs
Methodology for Application of 3-D Stresses to Surface Damage-Based Risk Assessment
SDM-12: Damage Detection and Evaluation I • Monday, 19 April 2004 • 1430 hrs
Three-Dimensional Analysis of Sandwich Panels with Common Defects
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
The Role of Force and Energy in Low Velocity Impact Events
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
Progressive Failure Simulation Under Random Vibration Loading Condition
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
Durability and Damage Tolerance Evaluation of the RLV
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
Stress Gradient Effects on Notched Composite Failure Using a Local-Global Approach
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
Interphasic Formulation for the Prediction of Delamination
SDM-39: Damage Detection and Evaluation II • Wednesday, 21 April 2004 • 0930 hrs
Vibration Isolator for Large Space Telescopes
SDM-46: Damping and Isolation • Wednesday, 21 April 2004 • 1430 hrs
Eigenvalue Sensitivity Based Topological Optimization for Passive Constrained Layer Damping
SDM-46: Damping and Isolation • Wednesday, 21 April 2004 • 1430 hrs
Automated Identification of Damping Treatment Characteristics
SDM-46: Damping and Isolation • Wednesday, 21 April 2004 • 1430 hrs
Characterization of a Lightweight, Low Frequency Acoustic Barrier with Spherical Particles
SDM-46: Damping and Isolation • Wednesday, 21 April 2004 • 1430 hrs
Accurate Evaluation of the Effects of Random Disorder on the Vibration Localization in Chains of Damped Oscillators
SDM-46: Damping and Isolation • Wednesday, 21 April 2004 • 1430 hrs
Dynamic Tailoring and Tuning for Precision Optical Space Structures
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
Strip Antenna Figure Errors due to Support Truss Member Length Imperfections
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
Analysis of Uncertainty Effects in Precision Mechanisms for Deployable Reflectors
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
Deployable Structures Based on the Bricard Linkages
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
New Tendon Reinforced Reflector for Large-Scale and Ultra-Lightweight Antenna Onboard the Satellite
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
Development of an Elastic Memory Composite Self-Locking Linear Actuator for Deployable Optics
SDM-13: Deployable Optical Structures • Monday, 19 April 2004 • 1430 hrs
Dynamic Wrinkle Reduction Strategies for Cable Suspended Membrane Structures
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
SALT: Second-order Augmentation of Latticed Trusses
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
Ultra Thin Deployable Reflector Antennas
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
Development of the Terrestrial Planet Finder Coronagraph Membrane V-Groove Sunshield
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
Undesired Equilibria of Self-deploying Pneumatic Envelopes
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
Buckling Analysis of Long Booms with Initial Geometric Imperfections
GSF-7: Design and Analysis of Gossamer Spacecraft • Tuesday, 20 April 2004 • 1400 hrs
Robust Design - An Important Tool for Business Success
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
A Robust & Secure System for Performing Engineering Analysis and Design in a Distributed Environment
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
A Distributed, Parallel, and Collaborative Environment for Design of Complex Systems
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
Parametric Modeling of Movables for Structural Analysis
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
Structural Response of a Supercavitating Torpedo Shell
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
Development of a Virtual D.O.F. Motion Platform for Simulation and Rapid Synthesis
SDM-40: Design Engineering I • Wednesday, 21 April 2004 • 0930 hrs
Towards Reusable Knowledge-Based Idealizations for Rapid Design and Analysis
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
A Substructuring Technique for Design Modifications of Interface Conditions
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
Formulation of the Optimal Latin Hypercube Design of Experiments Using a Permutation Genetic Algorithm
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
Shape Optimization via Mesh Elements
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
Simultaneous Topology and Curvilinear Fiber Path Design of Composite Layers Using Cellular Automata
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
Modeling R-curves of Aluminum Alloys New Numerical Models and Methods
SDM-58: Design Engineering II • Thursday, 22 April 2004 • 0930 hrs
Normal Constraint Method with Guarantee of Even Representation of Complete Pareto Frontier
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Adaptive Weighted Sum Method for Bi-objective Optimization
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Using Power of Ants for Optimization
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Morphing UAV Pareto Curve Shift for Enhanced Performance
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Evaluation of a Graphical Design Interface for Design Space Visualization
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Web-based Visualization Environment for Decision-Making in Multidisciplinary Design Optimization
SDM-24: Design Optimization Methods • Tuesday, 20 April 2004 • 0930 hrs
Structural Parameter Identification Using Robust Genetic Algorithm Optimization Method
SDM-59: Design Tradeoffs and Optimization • Thursday, 22 April 2004 • 0930 hrs
A Numerical Method for Cost-Weight Optimisation of Stringer-Skin Panels
SDM-59: Design Tradeoffs and Optimization • Thursday, 22 April 2004 • 0930 hrs
Parametric Modeling of Aircraft Families for Load Calculation Support
SDM-59: Design Tradeoffs and Optimization • Thursday, 22 April 2004 • 0930 hrs
Layup Optimization with GA for Tapered Laminates with Internal Plydrops
SDM-59: Design Tradeoffs and Optimization • Thursday, 22 April 2004 • 0930 hrs
A System Approach to Dynamic Response Variability Under Parameter Uncertainty and Variability
SDM-59: Design Tradeoffs and Optimization • Thursday, 22 April 2004 • 0930 hrs
A DMAP Program for the Selection of Accelerometer Locations in MSC/NASTRAN
SDM-4: Dynamic Modeling and Analysis • Monday, 19 April 2004 • 0930 hrs
A Direct Least Square Formulation of the KMA Method
SDM-4: Dynamic Modeling and Analysis • Monday, 19 April 2004 • 0930 hrs
Spectral Analysis Method for Linear Dynamic Systems
SDM-4: Dynamic Modeling and Analysis • Monday, 19 April 2004 • 0930 hrs
Random Eigenvalue Analysis of an Airframe
SDM-4: Dynamic Modeling and Analysis • Monday, 19 April 2004 • 0930 hrs
Statistical Comparison and Improvement of Methods for Combining Random and Harmonic Loads
SDM-4: Dynamic Modeling and Analysis • Monday, 19 April 2004 • 0930 hrs
Analytical Expressions of Modal Characteristics for Segmented Cylindrical Shell Vibration
SDM-25: Dynamics • Tuesday, 20 April 2004 • 0930 hrs
Vibration Modeling of Bladed Disks Subject to Geometric Mistuning and Design Changes
SDM-25: Dynamics • Tuesday, 20 April 2004 • 0930 hrs
Dynamic Impact Loading Damage Propagation in Composite Structures
SDM-25: Dynamics • Tuesday, 20 April 2004 • 0930 hrs
Composite Honeycomb Treatment via Non-Obstructive Particle Damping (NOPD)
SDM-25: Dynamics • Tuesday, 20 April 2004 • 0930 hrs
Sensitivity of Vehicle Vibrations to Subsystem Structural Variations
SDM-25: Dynamics • Tuesday, 20 April 2004 • 0930 hrs
Dynamics of an Axially Moving Viscoelastic Beam Subject to Axial Tension
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
An Extension of the Ghost Fluid Method for Coupling Fluids with Thin, Open Structures
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
Effect of Configuration Parameters on the Response and Stability of HAWT's
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
Linear Vibrations of Planar Prestressed Elastica Arches
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
Effects of Unsteady Pump Cavitation on Propulsion-Structure Interaction (Pogo) in Liquid Rockets
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
Spectral Element Model for the Pipelines with Internal Unsteady Flow
SDM-60: Dynamics of Coupled Systems • Thursday, 22 April 2004 • 0930 hrs
A Double-Distribution Statistical Algorithm for Composite Laminate Optimization
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
Variable Chromosome Length Genetic Algorithm for Structural Topology Design Optimization
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
A New Algorithm for Mixed-Discrete Design Optimization
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
A SAND Approach Based on Cellular Computation Models for Analysis and Optimization
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
Bone Structure Adaptation as a Cellular Automaton Optimization Process
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
Development of a Helicopter Blade FE Model Using MIGA Optimization
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
Dynamic Analysis and Parameter Optimization of a Fiber Optic Sensor Using Neural Networks
SDM-47: Evolutionary Computing Methods • Wednesday, 21 April 2004 • 1430 hrs
Approach to Identify Debonding in Soft-Core Sandwich Beams
SDM-5: Experimental Dynamics • Monday, 19 April 2004 • 0930 hrs
Modal Interactions in a Cantilever Plate: An Experimental Study
SDM-5: Experimental Dynamics • Monday, 19 April 2004 • 0930 hrs
Scanning Laser Doppler Vibrometry for Delamination Detection in Frescoes
SDM-5: Experimental Dynamics • Monday, 19 April 2004 • 0930 hrs
A Stress-Control-Based Live-Fire Ground Testing Methodology
SDM-5: Experimental Dynamics • Monday, 19 April 2004 • 0930 hrs
Panel Flutter Model Identification Using the Minimum Model Error Method. Part 1: Free Response
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Formulation of an Aircraft Structural Uncertainty Model for Robust Flutter Predictions
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Wind-Tunnel Model and a Controller for Flutter Suppression
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Flutter/Aeroelastic Response of Panels via a Combined Galerkin-Volterra Series Approach
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Time/Frequency Analysis of the Flutter of the Flexible HSCT Semispan Model
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Panel Flutter Model Identification Using the Minimum Model Error Method. Part 2: Forced Response
SDM-41: Flutter • Wednesday, 21 April 2004 • 0930 hrs
Laboratory Analysis of Polymer Thin Films for Planetary Balloons and Gossamer Structures
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
A Material Structural Performance Index for Strain Based Deloyable Trusses
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
Open-Celled Rigid Foams for Self-Deploying Foam Antenna Structures
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
PBO Braided Cord: Mechanical Properties Analysis for Aerospace Vehicles
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
Resin and Manufacturing Development for Light Curing Inflatable Composite Booms
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
Lightweight Shape Memory Self-Deployable Structures for Gossamer Applications
GSF-5: Gossamer Spacecraft Materials • Tuesday, 20 April 2004 • 0930 hrs
Measurement of Parabolic Cylindrical Reflectors in the DART Precision Test Bed
GSF-6: Gossamer Spacecraft Testing • Tuesday, 20 April 2004 • 0930 hrs
Photogrammetry and Videogrammetry Methods for Solar Sails and Other Gossamer Structures
GSF-6: Gossamer Spacecraft Testing • Tuesday, 20 April 2004 • 0930 hrs
Validation of Laser-Induced Fluorescent Photogrammetric Targets on Membrane Structures
GSF-6: Gossamer Spacecraft Testing • Tuesday, 20 April 2004 • 0930 hrs
Development of Modal Test Techniques for Validation of a Solar Sail Design
GSF-6: Gossamer Spacecraft Testing • Tuesday, 20 April 2004 • 0930 hrs
Development and Test of a Rigidizable Inflatable Structure Experiment
GSF-6: Gossamer Spacecraft Testing • Tuesday, 20 April 2004 • 0930 hrs
Variable Matrices Method for Self-identification of Adaptive Gyroscopic Structure Systems
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
Bolt Loosening Detection Method by Using Smart Washer Adopted 4SID
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
An Frequency Response Function-Based Damage Identification Method for Cylindrical Shell Structures
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
Embedded Ultrasonic Structural Radar with Piezoelectric Wafer Active Sensors for Damage Detection in Cylindrical Shell Structures
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
Structural Health Monitoring Using Macro-fiber Composites and Impedance Methods
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
A Fuzzy Finite Element Approach for the Analysis of Fiber-Reinforced Laminated Composite Beams
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
Health Prognostics of a Composite Patch Using a Stiffness-Energy Sensor
ASC-10: Health Monitoring • Thursday, 22 April 2004 • 0930 hrs
High Velocity Impacts of Man Portable Air Defense Systems (MANPADS) on Selected Targets
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
Testing Composite Joints Under High Energy Hydrodynamic Ram Conditions
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
A Gradient-Dependent Constitutive Model to Simulate Impact Damage Problem
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
Dislocation-Based Plasticity at High-Strain-Rates in Solids
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
Numerical Analysis for a Study of the Mitigation of Hypervelocity Gouging
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
Finite Element Simulation of Soft Projectile Impacting Braided Composite Structures
SDM-48: High Energy Impact Considerations • Wednesday, 21 April 2004 • 1430 hrs
Optical Strain Measurement of an Inflated Cylinder Using Photgrammetry with Application to Scientific Balloons
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Pressure-Augmented Near Net-Shape Membrane Mirror
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Development of a 7-Meter Inflatable Reflectarray Antenna
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Load Deflection Behaviour of Inflated Beams Made of Various Foil Materials
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Grid Sphere Electrodes Used for Current Collection at the Positive Pole of Electrodynamic Tethers
GSF-1: Inflatables • Monday, 19 April 2004 • 0930 hrs
Polynomial Chaos Expansion Applied to Airfoil Limit Cycle Oscillations
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
Modeling the LCO of a Delta Wing Using a High Fidelity Structural Model
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
Stability and Limit Cycle Oscillation Amplitude Prediction for Simple Nonlinear Aeroelastic Systems
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
Transonic Limit Cycle Flutter/LCO
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
A Direct Method for Quantifying Limit-Cycle Oscillation Response Characteristics in the Presence of Uncertainties
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach
SDM-26: Limit Cycle Oscillation • Tuesday, 20 April 2004 • 0930 hrs
Through-Laminate Damage in Cryogenically Cycled Polymer Composites
SDM-33: Materials in Cryogenic Environments I • Tuesday, 20 April 2004 • 1400 hrs
Parametric Analysis on the Adjacent Ply Crack Formation in Laminated Structures for Cryogenic Propellant Tank Application
SDM-33: Materials in Cryogenic Environments I • Tuesday, 20 April 2004 • 1400 hrs
Damage Development in Laminates Mechanically Cycled at Cryogenic Temperature
SDM-33: Materials in Cryogenic Environments I • Tuesday, 20 April 2004 • 1400 hrs
Virtual Testing Versus Physical Testing for Material Characterization
SDM-33: Materials in Cryogenic Environments I • Tuesday, 20 April 2004 • 1400 hrs
Hydrogen Permeability of Polymer Based Composites Under Bi-axial Strain and Cryogenic Temperatures
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Permeability and Life-time Durability of Polymer Matrix Composites for Cryogenic Fuel Tanks
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Modeling of Permeability and Damage in Graphite/epoxy Laminates at Cryogenic Temperatures
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Prediction of Leakage Rate Through Damage Network in Cryogenic Composite Laminates
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Numerical Modelling of Cryogen Leakage Through Composite Laminates
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Shortened Qualification Testing Time for Propellant Tanks of a Reusable Launch Vehicle
SDM-42: Materials in Cryogenic Environments II • Wednesday, 21 April 2004 • 0930 hrs
Selective Reinforcement to Improve Fracture Toughness and Fatigue Crack Growth Resistance in Metallic Structures
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Effects of Cell Shape and Strut Cross-Sectional Area Variations on the Elastic Properties of Three-Dimensional Open-Cell Foams
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Impact Response of Sandwich Beams with Functionally Graded Core
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Total Fatigue Life Prediction Growth Rate Models for FGI 1854 E-glass/Dow 510A-40 Vinyl Ester Composite Laminates
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Effects of Shape and Surface Area of Fiber in Short Fiber Composites
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Micromechanical Failure Analysis of Thin Plain Weave Textile Composites Using the Finite Element Method
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Comparative Study of Woven-Roving and Stitch-Bonded Composites Under Low Velocity Impact Loads
SDM-49: Mechanics of Materials • Wednesday, 21 April 2004 • 1430 hrs
Buckling and Shape Control of Composite Laminates Using Embedded Shape Memory Alloys Wires
ASC-1: Modeling and Simulation I • Tuesday, 20 April 2004 • 0930 hrs
Electro-thermo-elastic Formulation and Layer-by-layer Modeling of a Smart Beam with Piezoelectric Patches
ASC-1: Modeling and Simulation I • Tuesday, 20 April 2004 • 0930 hrs
A Simple Thermopiezoelastic Model for Composite Shells with Accurate Stress Recovery
ASC-1: Modeling and Simulation I • Tuesday, 20 April 2004 • 0930 hrs
Adaptive Control of Smart Space Structures Based on Artificial Potential Energy Method
ASC-1: Modeling and Simulation I • Tuesday, 20 April 2004 • 0930 hrs
Modeling of a Shape Memory Alloy Active Catheter
ASC-1: Modeling and Simulation I • Tuesday, 20 April 2004 • 0930 hrs
Coupled Finite Element for Non-linear Laminated Piezoelectric Composite Shells with Applications to Buckling and Postbuckling Behavior
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Analysis of Adaptive Sandwich Composite Beans with Piezoelectric Actuators and Sensors Using Coupled High-Order Layerwise Mechanics
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Dynamic Characterization of a Smart Composite Panel Using a Hybrid Approach
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Analysis, Design, and Structural-Aerodynamic Coupling of a Piezoelectric Active Fin
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Topology Design of Active Trusses with Energy Constraint
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Shape Optimization of Electrodes for Piezoelectric Actuators Dynamic Analysis
ASC-3: Modeling and Simulation II • Tuesday, 20 April 2004 • 1400 hrs
Comparison of Morphing Wing Stategies Based upon Aircraft Performance Impacts
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
Impact of Actuation Concepts on Morphing Aircraft Structures
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
A Multi-disciplinary Assessment of Morphing Aircraft Technology Applied to Tactical Cruise Missile Configuations
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
Aerodynamic and Aeroelastic Considerations of a Variable-Span Morphing Wing
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
Design and Wind-Tunnel Analysis of a Fully Adaptive Aircraft Configuration
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
Aircraft Structural Morphing Using Tendon Actuated Compliant Cellular Trusses
ASC-4: Morphing Aircraft Structures • Tuesday, 20 April 2004 • 1400 hrs
A Framework for Morphing Capability Assessment
ASC-2: Morphing Capability Panel • Tuesday, 20 April 2004 • 0930 hrs
An Aeroelastic Topology Optimization Approach for Adaptive Wing Design
ASC-5: Morphing Devices and Control • Wednesday, 21 April 2004 • 0930 hrs
A Morphing Concept Based on Unsymmetric Composite Laminates and Piezoceramic MFC Actuators
ASC-5: Morphing Devices and Control • Wednesday, 21 April 2004 • 0930 hrs
Morphing Inflatable Wing Development for Compact Package Unmanned Aerial Vehicles
ASC-5: Morphing Devices and Control • Wednesday, 21 April 2004 • 0930 hrs
Pneumatic Morphing Aspect Ratio Wing
ASC-5: Morphing Devices and Control • Wednesday, 21 April 2004 • 0930 hrs
Light Curing Rigidizable Inflatable Wing
ASC-5: Morphing Devices and Control • Wednesday, 21 April 2004 • 0930 hrs
Development of an Adaptive Stiffness All-Moving Vertical Tail
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
Experimental Validation of Wing Twist Control Using Adaptive Internal Structures
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
A Design and Analysis of a Morphing Hyper-Elliptic Cambered Span (HECS) Wing
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
Adaptive Aerostructures: Improving Militarily Enabled, High Performance Subscale UAVs
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
Air Vehicle Control Using Multiple Control Surfaces
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
Morphing Wing Structures for Loitering Air Vehicles
ASC-7: Morphing Structures Design and Testing • Wednesday, 21 April 2004 • 1430 hrs
Decomposition and Two-level Optimization of Structures with Discrete Sizing Variables
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
Value-Based Multidisciplinary Optimization for Commercial Aircraft Design
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
MDO Architectures for Coupled Aerodynamic and Structural Optimization of a Flexible Wing
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
Multidisciplinary Design Optimization for the Preliminary Design of Aeronautical Configurations
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
Spectral Level Set Methodology in MDO
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
Optimization of Trimmed Flight Configurations for Supercavitating Vehicles
SDM-6: Multidisciplinary Design Optimization • Monday, 19 April 2004 • 0930 hrs
Best PaperBest Paper
Constitutive Modeling of Crosslinked Nanotube Materials
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
Predicting the Influence of Nano-scale Material Structure on the In-plane Buckling of Orthotropic Plates
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
SWNT and MWNT Reinforced Carbon Nanocomposite Fibrils
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
Discrete Atomistic and Continuum Fracture Parameter Modeling of a Graphene Sheet
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
Carbon-Nanotube-Reinforced Energetic Nanocomposites: CNT Alignment Technique and Simulation
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
Estimation of Elastic Parameters of Nanoclay-Reinforced Polymers using Mean-Field Theory
SDM-14: Nanostructured Materials I • Monday, 19 April 2004 • 1430 hrs
An Empirical Molecular Dynamics Potential for an AI+FE2O3 Reactive Metal Powder Mixture
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
Deformation Mechanisms of Copper Nanowires Under Tensile Loading
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
Multiscale Modeling of Metallic Materials Containing Embedded Particles
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
Stress Distribution During Deformation of Polycrystalline Aluminum by Molecular-dynamics and Finite-element Modeling
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
Molecular Dynamics Simulations of Grain Boundary Decohesion in FCC Copper and Aluminum
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
A Grain Boundary Sliding Model for Nanocrystals
SDM-27: Nanostructured Materials II • Tuesday, 20 April 2004 • 0930 hrs
Compressive Strength Enhancement of Pultruded Thermoplastic Composites Using Nanoclay Reinforcement
SDM-34: Nanostructured Materials III • Tuesday, 20 April 2004 • 1400 hrs
Space Durable Polyimide/Carbon Nanotube Composite Films for Potential Applications on Gossamer Spacecraft
SDM-34: Nanostructured Materials III • Tuesday, 20 April 2004 • 1400 hrs
Anisotropic Elastic Properties of Carbon Nanotubes
SDM-34: Nanostructured Materials III • Tuesday, 20 April 2004 • 1400 hrs
Effective Elastic Properties of Carbon Nanotubes and Carbon Nanotube Reinforced Composites
SDM-34: Nanostructured Materials III • Tuesday, 20 April 2004 • 1400 hrs
Effects of Interfacial Friction on Composites Containing Nanotube Ropes
SDM-34: Nanostructured Materials III • Tuesday, 20 April 2004 • 1400 hrs
Probabilistic Risk Assessment of Joints with Cold-worked Holes
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
A Probabilistic Treatment of Conflicting Expert Opinion
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Application of Parallel Processing to Probabilistic Fracture Mechanics Analysis of Gas Turbine Disks
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Dynamic Thermal Stress Creep Buckling of Linear Viscoelastic Columns - Probabilistic Failures and Survival Times
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Random Eigenvalue Problems in Structural Dynamics
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Non Deterministic Approaches for the Evaluation of the Mistune Effects on the Rotor Dynamics
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Statistical Approaches to Structural-acoustics
NDA-4: NDA Applications I • Tuesday, 20 April 2004 • 1400 hrs
Experiences with Probabilistic Analysis Applied to Controlled Systems
NDA-7: NDA Applications II • Thursday, 22 April 2004 • 0930 hrs
A Methodology for Probabilistic Creep-Fatigue Life Assessment of Hot Gas Path Components
NDA-7: NDA Applications II • Thursday, 22 April 2004 • 0930 hrs
Development and Illustration of Model Validation Concepts from an Applied Modeling Perspective
NDA-7: NDA Applications II • Thursday, 22 April 2004 • 0930 hrs
Stochastic Finite Element Modelling of Fibre-Metal Laminates
NDA-7: NDA Applications II • Thursday, 22 April 2004 • 0930 hrs
Using Random Set Theory to Calculate Reliability Bounds in Situations of Little Information: An Application to a Finite Element Intermediate Complexity Wing Model
NDA-2: NDA Methods I • Monday, 19 April 2004 • 1430 hrs
A New Probabilistic Method for Use in Vibro-Acoustic Analysis
NDA-2: NDA Methods I • Monday, 19 April 2004 • 1430 hrs
Discrete Design Optimization Under Uncertainty: A Generalized Population-Based Sampling Genetic Algorithm
NDA-2: NDA Methods I • Monday, 19 April 2004 • 1430 hrs
A Framework to Estimate Uncertain Random Variables
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
Adaptive Optimal Sampling Methodology for Zone-Based Probabilistic Life Prediction
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
Empirical Modeling Based on Neural Networks and Bayesian Learning
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
Improving Accelerated Corrosion Test Predictions Using Linear Polarization Resistance Sensors with Neural Networks
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
NESSUS Capabilities for Ill-Behaved Performance Functions
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
Bayesian Models for the Reliability Analysis of Composite Plates
NDA-5: NDA Methods II • Wednesday, 21 April 2004 • 0930 hrs
Evolution of Structures Design Philosophy and Criteria
SDM-35: New Approaches for Aircraft Structures Certification • Tuesday, 20 April 2004 • 1400 hrs
A Hybrid Probabilistic Method for Composite Aircraft Design
SDM-35: New Approaches for Aircraft Structures Certification • Tuesday, 20 April 2004 • 1400 hrs
A Functional Methodology for Assessing Post-Initation Damage in Composite Structures and Bonded Joints
SDM-35: New Approaches for Aircraft Structures Certification • Tuesday, 20 April 2004 • 1400 hrs
Probabilistic Damage Tolerance Methodology for Reliability Design and Inspection Optimization
SDM-35: New Approaches for Aircraft Structures Certification • Tuesday, 20 April 2004 • 1400 hrs
Thermal-Structural Optimization of Integrated Cryogenic Propellant Tank Concepts for a Reusable Launch Vehicle
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Trade Study Results for a Second-Generation Reusable Launch Vehicle Composite Hydrogen Tank
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Prediction of Micro-crack Densities in Cryogenic IM7/977-2 Propellant Tanks
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
A Multiscale Approach to the Effects of Cryogenic Environments on Polymer Matrix Composites
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Analysis of TPS Sandwich Panel with Foam Core
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Polyimide Foam Development and Characterization for Lightweight Integrated Structures
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Fracture Properties Estimation of Aluminum Lithium Alloys Subjected to Exposure Time (Analytical Approach Versus Physical Testing)
SDM-50: Next Generation RLV Cryogenic Propellant Tanks and Integrated Structures • Wednesday, 21 April 2004 • 1430 hrs
Nonlinear Aeroelastic Modeling by Block-Oriented Identification
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Volterra Kernel Identification and Extrapolation for the F/A-18 Active Aeroelastic Wing
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Non-linear Phenomena Analysis of Stall-induced Aeroelastic Oscillations
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Identification of a Nonlinear Aeroelastic Aircraft Wing Model
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
The Effects of External Stores on Nonlinear Aeroelastic Responses
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Nonlinear Aeroelastic Behavior of a High Flexibility Wing with Long Span Considering Large Deflection
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects
SDM-51: Nonlinear Aeroelasticity • Wednesday, 21 April 2004 • 1430 hrs
Nonlinear Interactions in the Responses of Heated Annular Plates
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
Predicting Uncertainty Propagation in a Highly Nonlinear System with a Stochastic Projection Method
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
Responses' Convergence for Time Integration of Highly Nonlinear Dynamic Models
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
Nonlinear Stiffness Estimation for Modal Finite Element Approach to Free Vibrations of Shallow Shells
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
On the Measures for Evaluating Time Discretized Operators and the Consequences Leading to Improved Algorithms by Design for Structural Dynamics
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
Nonlinear Magneto-Thermo-Elastic Laminated Composite Plates: Modeling and Vibrational Behavior
SDM-15: Nonlinear Analysis • Monday, 19 April 2004 • 1430 hrs
Simple Discrete Lumped Parameter Models: Insight Into Large Displacement Continuous Beam Models
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
Forced Non-linear Vibration of Cylindrical Laminated Shells by the p-version Finite Element Method
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
Nonlinear Dynamics of a Buckling Beam Actuator
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
Nonlinear Vibrations of a Satellite Truss Structure with Gaps
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
Transient Geometrically Nonlinear Analysis of Polar Orthotropic Circular Plates Using the Rayleigh Ritz Method
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
Large Lateral Displacement Beam Models Using Continuous Shape Functions
SDM-43: Nonlinear Modeling Methods • Wednesday, 21 April 2004 • 0930 hrs
A Unilevel Method for Reliability Based Design Optimization
SDM-61: Probabilistic Methods and Reliability Based Optimization • Thursday, 22 April 2004 • 0930 hrs
Numerical Experiments of Reliability-Based Optimization Methods
SDM-61: Probabilistic Methods and Reliability Based Optimization • Thursday, 22 April 2004 • 0930 hrs
Reliability Optimization of Structures Using Probabilistic Sufficiency Factor And Correction Response Surface
SDM-61: Probabilistic Methods and Reliability Based Optimization • Thursday, 22 April 2004 • 0930 hrs
Simulation Model of an Autonomous Underwater Vehicle for Design Optimization
SDM-61: Probabilistic Methods and Reliability Based Optimization • Thursday, 22 April 2004 • 0930 hrs
Handling Bifurcations in the Optimal Design of Transient Dynamic Problems
SDM-61: Probabilistic Methods and Reliability Based Optimization • Thursday, 22 April 2004 • 0930 hrs
Evaluation of Piezoelectric PVDF Polymers for Use in Space Environments
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Optimization of Piezo-Electric PVDF Polymers for Adaptive Optics in Space Environments
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Rapid Consolidation of Gamma-TiAl Intermetallics via Plasma Pressure Compaction
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Carbon Nanotube Electrode Films for Gas Sensing
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Fretting of Single Crystal/Polycrystalline Nickel Contacts at Elevated Frequency and Temperature
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Experimental Verification of the Characterization of Material Microyield
SDM-7: Processing and Testing of Materials • Monday, 19 April 2004 • 0930 hrs
Reinvestigation of Nonlinear Random Response of Shallow Shells Using Finite Element Modal Formulation
SDM-8: Random Vibration and Nonlinear Dynamics • Monday, 19 April 2004 • 0930 hrs
The Effect of Basis Selection on Thermal-Acoustic Random Response Prediction Using Nonlinear Modal Simulation
SDM-8: Random Vibration and Nonlinear Dynamics • Monday, 19 April 2004 • 0930 hrs
Enhanced Nonlinear Dynamics for Accurate Identification of Stiffness Loss in a Thermo-Shielding Panel
SDM-8: Random Vibration and Nonlinear Dynamics • Monday, 19 April 2004 • 0930 hrs
Prediction of the Dynamic Response and Fatigue Life of Panels Subjected to Thermo-Acoustic Loading
SDM-8: Random Vibration and Nonlinear Dynamics • Monday, 19 April 2004 • 0930 hrs
Nonlinear Random Response of Shallow Shells at Elevated Temperatures Using Finite Element Modal Method
SDM-8: Random Vibration and Nonlinear Dynamics • Monday, 19 April 2004 • 0930 hrs
An Efficient Model Reduction Method for Linear Dynamic Systems with Multiple Inputs
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
An Efficient Approach for Solving Nonlinear Aeroelastic Phenomenona Using Reduced-Order Modeling
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
Reduced Structural Modeling of Integrally-Strained Slender Wings
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
A Reduced-Order Model for Electrically Actuated Microplates
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
Aeroelastic Model Reduction for an Affordable CFD Based Flutter Analysis
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
Numerical Conditioning and Reduction of Large Spacecraft Models for Dynamic Analysis
SDM-62: Reduced Order Modeling • Thursday, 22 April 2004 • 0930 hrs
Non-Deterministic Optimization of Composite Structures Reliability
NDA-6: Reliability • Wednesday, 21 April 2004 • 1430 hrs
Improved Component Reliability Assessments Using Joint Probability Modeling
NDA-6: Reliability • Wednesday, 21 April 2004 • 1430 hrs
Reliability-Based Global Optimization of Stiffened Panels Using Probabilistic Sufficiency Factor
NDA-6: Reliability • Wednesday, 21 April 2004 • 1430 hrs
Multi-Objective Reliability-Based Optimization
NDA-6: Reliability • Wednesday, 21 April 2004 • 1430 hrs
Efficient Reliability-Based Structural Optimization Through Most Probable Failure Point Approximation
NDA-6: Reliability • Wednesday, 21 April 2004 • 1430 hrs
A Consistent Dissipative Time Integration Scheme for Structural Dynamics: Application to Rotordynamics
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
Identification and Updating of AB204 Helicopter Blade F.E. Model by Means of Static and Dynamic Tests
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
Design and Testing of a Compact Fluidic Layered Isolator for High-Frequency Helicopter Gearbox Isolation
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
The HHC Algorithm for Helicopter Vibration Reduction Revisited
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
A 3-D Flutter Model for Rotor Blades with Trailing-Edge Flaps
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
Helicopter Blade Lag Damping Using Embedded Fluid Elastic Inertial Dampers
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
Swashplateless Helicopter Rotor System with Active Trailing-Edge Flaps for Primary and Vibration Controls
SDM-52: Rotorcraft Applications • Wednesday, 21 April 2004 • 1430 hrs
Nonlinear Simulation of Piezoceramic Materials Using Micromechanical Approach
ASC-6: Smart Sensors and Actuators I • Wednesday, 21 April 2004 • 0930 hrs
Micro- and Nano-sensors and Their Potential Applications in Military Adaptive Structures
ASC-6: Smart Sensors and Actuators I • Wednesday, 21 April 2004 • 0930 hrs
Hyperhelical Actuators: Coils and Coiled-Coils
ASC-6: Smart Sensors and Actuators I • Wednesday, 21 April 2004 • 0930 hrs
An Adaptive Structures Electro-mechanical Device for Dynamic Flow Control Applications
ASC-6: Smart Sensors and Actuators I • Wednesday, 21 April 2004 • 0930 hrs
Anisotropic Piezocomposite Actuator Incorporating Machined PMN-PT Single Crystal Fibers
ASC-8: Smart Sensors and Actuators II • Wednesday, 21 April 2004 • 1430 hrs
Design and Development of Piezoelectric Inchworm Actuator
ASC-8: Smart Sensors and Actuators II • Wednesday, 21 April 2004 • 1430 hrs
Nondimensional Analysis of Electrorheological Dampers Using an Eyring Constitutive Relationship
ASC-8: Smart Sensors and Actuators II • Wednesday, 21 April 2004 • 1430 hrs
Adaptive Sensors for Aircraft Operational Monitoring
ASC-8: Smart Sensors and Actuators II • Wednesday, 21 April 2004 • 1430 hrs
Engineering Development Model Testing of the PowerSphere
GSF-3: Solar Arrays and Concentrators • Monday, 19 April 2004 • 1430 hrs
Deployable Structures Space Science Experiment for Large Aperture, High Power Missions in MEO
GSF-3: Solar Arrays and Concentrators • Monday, 19 April 2004 • 1430 hrs
Power-Scalable Inflation-Deployed Solar Arrays
GSF-3: Solar Arrays and Concentrators • Monday, 19 April 2004 • 1430 hrs
Best PaperBest Paper
New Deployable Reflector Concept
GSF-3: Solar Arrays and Concentrators • Monday, 19 April 2004 • 1430 hrs
Flight Testing of an Inflatable and Rigidizable Structure
GSF-3: Solar Arrays and Concentrators • Monday, 19 April 2004 • 1430 hrs
The Development of Solar Sail Propulsion for NASA Science Missions
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
Development and Ground Testing of a Compactly Stowed Inflatably Deployed Solar Sail
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
Innovative Structural Design Features for a 10m Solar Sail Demonstrator
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
Parametric Studies of Square Solar Sails Using Finite Element Analysis
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
Design Considerations for an Integrated Solar Sail Diagnostics System
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
A Preliminary Investigation of a Spin-Stabilized Solar Sail
GSF-2: Solar Sails I • Monday, 19 April 2004 • 0930 hrs
Robert L. Forward's Solar Photon Thruster Solar Sail Architecture Revisited
GSF-4: Solar Sails II • Monday, 19 April 2004 • 1430 hrs
Experimental and Numerical Correlation of Gravity Sag In Solar Sail Quality Membranes
GSF-4: Solar Sails II • Monday, 19 April 2004 • 1430 hrs
Simulating Nonlinear Deformations of Solar Sail Membranes Using Explicit Time Integration
GSF-4: Solar Sails II • Monday, 19 April 2004 • 1430 hrs
A Simplified Vibration Model of Solid Rocket Motor Coupled with Solid Propellant
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Rigid Body Mode Control of Free-Free Launcher Structural Models in Gravity Fields
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
A Dynamic Characteristics Prediction of Large Satellite Antennas by Component Tests
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Coupled Thermo-Structural Analysis of an Earth Orbiting Flexible Structure
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Component in the Loop Model Verification for Large Precision Spacecraft Structures
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Mars Exploration Rover Airbag Landing Loads Testing and Analysis
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Hybrid Interface Modal Model Formulation for Launch Vehicle Coupled Loads Analysis
SDM-36: Spacecraft and Launch Vehicle Dynamics • Tuesday, 20 April 2004 • 1400 hrs
Modeling, Analysis and Testing of some Deployable/Inflatable Structures
SDM-37: Spacecraft Applications • Tuesday, 20 April 2004 • 1400 hrs
Variational Coupled Loads Analyses: Reducing Risk in the Development of Space-Flight Hardware
SDM-37: Spacecraft Applications • Tuesday, 20 April 2004 • 1400 hrs
Compliant Joints for On-orbit Remote Berthing and Structural Attachment of Large Space Structures
SDM-37: Spacecraft Applications • Tuesday, 20 April 2004 • 1400 hrs
Launch Loads Development Using Sine Vibration Methodology
SDM-37: Spacecraft Applications • Tuesday, 20 April 2004 • 1400 hrs
Static Testing of an Inflatable/Rigidizable Hexapod Structure
SDM-37: Spacecraft Applications • Tuesday, 20 April 2004 • 1400 hrs
Nonlinear Flutter of Cylindrical Shell Panels Under Yawed Supersonic Flow Using FE
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Wind Tunnel to Atmospheric Mapping for Static Aeroelastic Scaling
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Aircraft Buffet Prediction Using Unsteady Aerodynamic Wind Tunnel Model Six-Component Balance Data
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Numerical Simulation of Nonslender Delta Wing Buffet at High Angle of Attack
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling
SDM-63: Special Topics in Aeroelasticity • Thursday, 22 April 2004 • 0930 hrs
Numerical and Experimental Dynamic Characteristics of Thin-Film Membranes
SDM-16: Special Topics in Dynamics • Monday, 19 April 2004 • 1430 hrs
Free Non-Axisymmetric Vibrations of Composite Full Cylindrical Shells with a Bonded Non-Central (or Eccentric) Single Lap Joint
SDM-16: Special Topics in Dynamics • Monday, 19 April 2004 • 1430 hrs
Free Vibration and Damping Characterization of Delaminated Composites by FEM
SDM-16: Special Topics in Dynamics • Monday, 19 April 2004 • 1430 hrs
Measurements and Modeling of Variability in the Dynamics of a Bolted Joint
SDM-16: Special Topics in Dynamics • Monday, 19 April 2004 • 1430 hrs
Magneto-Elastodynamic Effects on Stress and Displacement Distributions of Cracked Electroconductive Plates
SDM-16: Special Topics in Dynamics • Monday, 19 April 2004 • 1430 hrs
Probabilistic Formulations to Robust Optimal Control
NDA-3: Stochastic Design • Tuesday, 20 April 2004 • 0930 hrs
Inverse Design for a Priori Specified Reliability
NDA-3: Stochastic Design • Tuesday, 20 April 2004 • 0930 hrs
Safety Factor and Inverse Reliability Measures
NDA-3: Stochastic Design • Tuesday, 20 April 2004 • 0930 hrs
Quantification of Uncertainty Using Inverse Methods
NDA-3: Stochastic Design • Tuesday, 20 April 2004 • 0930 hrs
A Study of Vehicle Structural Layouts in Post-WWII Aircraft
SDM-17: Structural Applications • Monday, 19 April 2004 • 1430 hrs
Design and Test of Full-Scale VARTM Integrally Stiffened CAI Cockpit Tub
SDM-17: Structural Applications • Monday, 19 April 2004 • 1430 hrs
Testing of a Delta IV Payload Attach Fitting (PAF) Substructure with an Integral Composite Flange
SDM-17: Structural Applications • Monday, 19 April 2004 • 1430 hrs
Design of a Combined Loads Machine for Tests on Fuselage Barrels and Curved Panels
SDM-17: Structural Applications • Monday, 19 April 2004 • 1430 hrs
Why are Airplanes so Safe Structurally? Effect of Various Safety Measures on Structural Safety of Aircraft
SDM-17: Structural Applications • Monday, 19 April 2004 • 1430 hrs
Primary Resonance Excitation of Electrically Actuated Clamped Circular Plates
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Vibration Control of Box Structures Using Multiple Piezo-Actuators and Sensors
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Multi-Harmonic Adaptive Vibration Control of Magnetic Bearing-Driveline with Auxiliary Feedback: Theory and Experiment
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Pseudo-Active Control of Helicopter Blade Vibration Using Piezoelectric Actuators
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Control of Flexible Aircraft Executing Time-Dependent Maneuvers
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Reduction of Random Response of Composite Plates Using Shape Memory Alloy in Thermal Environments
SDM-18: Structural Control • Monday, 19 April 2004 • 1430 hrs
Damage Detection Capabilities Based on New Signal Processing Approach
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
A Probabilistic Damage-Based Approach to Structural Health Management
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
Finite Element Modeling for Piezoelectric Smart Composites Including Debonding
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
An Integrated Active Sensing System for Damage Identification and Prognosis
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
Optimal Sensor Placement for Damage Characterization Using Genetic Algorithms
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
Development of Piezoelectric Acoustic Sensors and Bio-Inspired Embedded Sensor Array Architecture for Structural Health Monitoring
SDM-53: Structural Health Management • Wednesday, 21 April 2004 • 1430 hrs
Global-Local Finite Element Analysis of Bonded Single-Lap Joints
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Nonlinear Analysis of Bonded Composite Single-Lap Joints
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Comparisons of Measured Moiré Fringe Surface Strains and Model Predictions for a Co-bonded Pi-Preform Composite Tee Joint
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Correlation of an Analysis Tool for 3-D Reinforced Bonded Joints on the F-35 Joint Strike Fighter
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Analysis of Adhesively Bonded Composite Joints Using a Higher-Order Theory
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Characterization of Transverse Impact Damage on Adhesively Bonded Glass/Epoxy Composite Joints
SDM-9: Structural Joining and Repair I • Monday, 19 April 2004 • 0930 hrs
Combined In-Plane and Through-the-Thickness Analysis for Failure Prediction of Bolted Composite Joints
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
Evaluation of Static Compression Properties of Notched Stitched Sandwich Structures
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
Experimental Investigation on Performance of Angle-Stitched Sandwich Structures
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
Design Curves for Metallic Z-Pinned Composite Laminated Double Cantilever Beams
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
An Efficient Interface/Joint Design for Dissimilar Materials and Structures
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
Differentiation of Damage and Failure Mechanisms of Co-Cured Fiber-Reinforced Composite Joints Using Acoustic Emission
SDM-28: Structural Joining and Repair II • Tuesday, 20 April 2004 • 0930 hrs
A Study of the Compession Mechanics of Soft-Resin Composites
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
Integrated Micromechanical-Structural Models for Long-term Behavior of FRP Composite Structures
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
Implementation of Higher Order Laminate Theory Into Strain Rate Dependent Micromechanics Analysis of Polymer Matrix Composites
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
The Effect of Strain Rate on Interlaminar Shear Properties
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
Size Effects in the Crushing of Honeycomb Structures
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
Biaxial Strength Measurements of IM7/977-2 Carbon/Epoxy Laminates Using Tabbed Cruciform Specimens
SDM-19: Structural Mechanics • Monday, 19 April 2004 • 1430 hrs
Alternate Formulations for Structural Optimization
SDM-20: Structural Optimization • Monday, 19 April 2004 • 1430 hrs
Combined Direct/Adjoint Reduced-Order Approximations for Design-Oriented Structural Acoustics
SDM-20: Structural Optimization • Monday, 19 April 2004 • 1430 hrs
Multigrid Accelerated Cellular Automata for Structural Design Optimization: A 1-D Implementation
SDM-20: Structural Optimization • Monday, 19 April 2004 • 1430 hrs
An Analytical Directional Growth Topology Parameterization to Enforce Manufacturing Requirements
SDM-20: Structural Optimization • Monday, 19 April 2004 • 1430 hrs
Load Updating for Nonlinear Finite Element Models
SDM-20: Structural Optimization • Monday, 19 April 2004 • 1430 hrs
Optimal Polymer Sheeting Die Design for Multiple Operation Conditions
SDM-54: Structural Optimization Applications • Wednesday, 21 April 2004 • 1430 hrs
Finite Element Analysis and Sizing Optimization of an Advanced Design Concept for a Composite Sail Structure
SDM-54: Structural Optimization Applications • Wednesday, 21 April 2004 • 1430 hrs
Shape Optimization of Steel Standard Profiles
SDM-54: Structural Optimization Applications • Wednesday, 21 April 2004 • 1430 hrs
Parameter Estimation of Spacecraft Fuel Slosh Model
SDM-54: Structural Optimization Applications • Wednesday, 21 April 2004 • 1430 hrs
Approximate Solution and Optimum Design for Postbuckling of Infinite Laminated Composite Plates Subjected to Compression Loading
SDM-10: Structural Stability and Postbuckling Behavior I • Monday, 19 April 2004 • 0930 hrs
An Experimental Investigation on the Post-buckling Behavior of Composite Stiffened Panels
SDM-10: Structural Stability and Postbuckling Behavior I • Monday, 19 April 2004 • 0930 hrs
Post-Buckling and Fatigue Limit of Artificially Delaminated Composites
SDM-10: Structural Stability and Postbuckling Behavior I • Monday, 19 April 2004 • 0930 hrs
Plastic Thermal Buckling of Uniformly Heated Bars with Temperature-Dependent Material Properties
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
Thermal Buckling of Metal Foam Sandwich Panels for Actively Cooled Thermal Protection Systems
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
Torsional Buckling of Thin-Walled Cylinders Under Circumferentially Varying Thermal Loads
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
On a Verified High-Fidelity Analysis for Axially Compressed Cylindrical Shells
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
Effects of Elastic Edge Restraints and Prestress on the Buckling Response of Compression-loaded Composite Panels
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
Buckling of Composite Plates with a Reinforced Circular Cutout Subjected to Uniform and Non-Uniform Compression
SDM-29: Structural Stability and Postbuckling Behavior II • Tuesday, 20 April 2004 • 0930 hrs
Selective Reinforcement to Enhance the Structural Performance of Metallic Compression Panels
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
Stiffened Panels in Compression: Redirecting Loads Toward High-Strength Stiffeners
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
Approximate Solution for the Compression Buckling of Fully-Anisotropic Cylindrical Shells
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
On Optimisation of Long Anisotropic Flat Plates Subject to Shear Buckling Loads
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
Parametric Design Curves for Shear Buckling of Flat Orthotropic Stiffened Panels with Application to Glare Material
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
Optimum Design of Filament-Wound Laminated Conical Shells for Buckling Using a Response Surface Methodology
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
Test and Analysis of a Composite Multi-bay Fuselage Panel Under Uni-axial Compression
SDM-64: Structural Stability and Postbuckling Behavior III • Thursday, 22 April 2004 • 0930 hrs
An Efficient Successive Reanalysis Technique for Engineering Structures
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
Convergent Nonparametric Variable Screening and Metamodeling Methods
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
Response Surface Optimization with Discrete Variables
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
An Efficient Strategy for Global Optimization Using Local Kriging Approximations
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
Efficiency Improvement of Response Surface Building Using Fast Reanalysis Methods
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
Preliminary Evaluation of a Hierarchical Metamodeling Technique for Systems with a Large Number of Parameters
SDM-44: Surrogate Models and Approximations Based Optimization • Wednesday, 21 April 2004 • 0930 hrs
Review of Space Shuttle Meteoroid/Orbital Debris Critical Risk Assessment Practices
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
The Use of Design of Experiments Methodology in a Modeling and Simulation World
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
Comparison of SPHC Hydrocode Results with Penetration Equations and Results of Other Codes
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
Tethers as Debris: Simulating Impacts of Tethers Fragments on Shuttle Tiles
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
Hypervelocity Impact of Orbital Debris on Thin Aluminum Plates
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
Foam-on-Tile Impact Modeling for the STS-107 Investigation
SDM-45: Survivability I • Wednesday, 21 April 2004 • 0930 hrs
C-130J Live Fire Test & Evaluation Program Test Results and Preparations for the C-130J Engine Nacelle Fire Extinguishing Evaluation
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Development Testing for Aircraft Dry Bay Suppression Using DXP
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Design of Negative Poisson's Ratio Materials Using Topology Optimization
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Sixth-Order Fitted Closure Methods for Shot-Fiber Reinforced Polymer Composite Systems
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Prediction of Spectrum Fatigue Crack Growth in Latest Generation High Damage Tolerance Alloys
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Mixed-mode Stress Intensity Factors for a Crack in an Anisotropic Bi-material Strip
SDM-55: Survivability II • Wednesday, 21 April 2004 • 1430 hrs
Integrated Survivability Assessment (ISA) in the Acquisition Lifecycle
SDM-65: Survivability III • Thursday, 22 April 2004 • 0930 hrs
Joint Aircraft Survivability Program - What's New
SDM-65: Survivability III • Thursday, 22 April 2004 • 0930 hrs
Finite Element Simulation of Ballistic Impact in Survivability Studies
SDM-65: Survivability III • Thursday, 22 April 2004 • 0930 hrs
Performance of Gen IV LSP for Thick Section Airfoil Damage Tolerance
SDM-65: Survivability III • Thursday, 22 April 2004 • 0930 hrs
Improved Infrared Countermeasures with Ultrafine Aluminum
SDM-65: Survivability III • Thursday, 22 April 2004 • 0930 hrs
Zero- and One-g Comparison of Ripple Amplitude in Single-Curved Parabolic Membranes Using Photogrammetry
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs
Study of Ripple Formation in Unidirectionally-Tensioned Membranes
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs
Dynamic Wrinkling Analysis of Kapton Membrane Under Tensile Loading
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs
Toward Effective Shell Modeling of Wrinkled Thin-Film Membranes Exhibiting Stress Concentrations
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs
Quantifying Square Membrane Wrinkle Behavior Using MITC Shell Elements
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs
A Spectrum Evaluation Method for Wrinkled Membranes Using Two-Dimensional Fast Fourier Transform
GSF-8: Wrinkling • Tuesday, 20 April 2004 • 1400 hrs