Table of Contents
Structure-Process-Property Study of Aligned Carbon Nanotube Interlaminar Reinforcement in Woven Carbon Fiber Prepreg Laminate
AIAA 2016-0148
Nanostructured Materials I • Monday, 4 January 2016 • 0900 hrs
Woven Hierarchical Aerospace Composite Laminates with Aligned Carbon Nanotube Bulk Reinforcement
AIAA 2016-0149
Nanostructured Materials I • Monday, 4 January 2016 • 0930 hrs
Nanoparticle Alignment using Oscillating Magnetic Fields for Scalable Nanocomposite Manufacturing
AIAA 2016-0150
Nanostructured Materials I • Monday, 4 January 2016 • 1000 hrs
Influence of Waviness on the Elastic Properties of Aligned Carbon Nanotube Polymer Matrix Nanocomposites
AIAA 2016-0151
Nanostructured Materials I • Monday, 4 January 2016 • 1030 hrs
Thermal conductivity via atomistic modeling for epoxy-SWNT composites
AIAA 2016-0152
Nanostructured Materials I • Monday, 4 January 2016 • 1100 hrs
Mode I Fracture Toughness of Aligned Carbon Nanotube Epoxy Nanocomposites
AIAA 2016-0153
Nanostructured Materials I • Monday, 4 January 2016 • 1130 hrs
Non-covalent Functionalization of CNT and Graphene and Its Application to Hybrid Carbon/Epoxy Composites
AIAA 2016-0154
Nanostructured Materials I • Monday, 4 January 2016 • 1200 hrs
Multiscale Modeling of Effective Piezoresistivity in Nanocomposite Bounded Explosives
AIAA 2016-0155
Fatigue & Fracture I • Monday, 4 January 2016 • 0900 hrs
Utilization of a Linear Solver for Multiscale Design and Optimization of Microstructures in an Airframe Panel Buckling Problem
AIAA 2016-0156
Fatigue & Fracture I • Monday, 4 January 2016 • 0930 hrs
High-energy hydroforming for the aerospace industry
AIAA 2016-0157
Fatigue & Fracture I • Monday, 4 January 2016 • 1000 hrs
Flight Vehicle Structural Design Processes for a Common Bulkhead and an MPCV Spacecraft Adapter
AIAA 2016-0158
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 0900 hrs
Performance Evaluation of a Morphing Trailing Edge Using Multipoint Aerostructural Design Optimization
AIAA 2016-0159
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 0930 hrs
Aerostructural Optimization of a Low Sweep Transonic Wing with Shock Control Bump
AIAA 2016-0160
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 1000 hrs
Cure Rate Tailoring of Thick Composites Via Temperature Controlled Vascular Pathways
AIAA 2016-0161
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 1030 hrs
Co-Design of Strain-Actuated Solar Arrays for Precision Pointing and Jitter Reduction
AIAA 2016-0162
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 1100 hrs
Adaptive Variable-Fidelity Analysis and Design for A Tailless Aircraft with Innovative Control Effectors under Model-Form Uncertainty
AIAA 2016-0163
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 1130 hrs
Aerodynamic Optimisation of Non-planar Lifting Surfaces
AIAA 2016-0164
Aero & Structural Technology Investigations • Monday, 4 January 2016 • 1200 hrs
Joining 3-D Finite Elements to Variational Asymptotic Beam Models
AIAA 2016-0200
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 0900 hrs
Constrained-Energy Cross-Well Actuation of the Duffing-Holmes Oscillator
AIAA 2016-0201
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 0930 hrs
The Evaluation of an Icosahedron' Eigenvalue
AIAA 2016-0202
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 1000 hrs
Evaluating the stiffness of conic interfacing parts : a practical method for finite element model updating based on experimental modal testing
AIAA 2016-0203
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 1030 hrs
Force Reconstruction from Ejection Tests of Aircraft Stores Used for Model Predictions and Missing/Bad Gages
AIAA 2016-0204
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 1100 hrs
Towards a Fluid-Structure Interaction Solver for Problems with Large Deformations Within the Open-Source SU2 Suite
AIAA 2016-0205
Structural Dynamic Modeling and Analysis • Monday, 4 January 2016 • 1130 hrs
Toward broadband resistive-inductive piezoelectric energy harvesters
AIAA 2016-0206
Energy Harvesting • Monday, 4 January 2016 • 0900 hrs
The Role of Sweep Rate in Energy Harvesting
AIAA 2016-0207
Energy Harvesting • Monday, 4 January 2016 • 0930 hrs
Representation and comparative study of electromagnetic-piezoelectric galloping energy harvesters
AIAA 2016-0208
Energy Harvesting • Monday, 4 January 2016 • 1000 hrs
Piezoaeroelastic investigation on the control and energy harvesting of galloping systems
AIAA 2016-0209
Energy Harvesting • Monday, 4 January 2016 • 1030 hrs
Energy Harvesting From Aeroelastic Instabilities
AIAA 2016-0210
Energy Harvesting • Monday, 4 January 2016 • 1100 hrs
Enhanced stability identi cation and global response prediction of galloping energy harvesters
AIAA 2016-0211
Energy Harvesting • Monday, 4 January 2016 • 1130 hrs
Conceptual Design and Structural Optimization of NASA Environmentally Responsible Aviation (ERA) Hybrid Wing Body Aircraft
AIAA 2016-0229
Aircraft Structural Design I • Monday, 4 January 2016 • 0900 hrs
Moving Aerospace Structural Design Practice to a Load and Resistance Factor Approach
AIAA 2016-0230
Aircraft Structural Design I • Monday, 4 January 2016 • 0930 hrs
A Historical Assessment of Building Block Development Test Programs for Modern Military Aircraft
AIAA 2016-0231
Aircraft Structural Design I • Monday, 4 January 2016 • 1000 hrs
Structural Loads Analysis of a Carrier Onboard Delivery Aircraft
AIAA 2016-0232
Aircraft Structural Design I • Monday, 4 January 2016 • 1030 hrs
Load Paths Visualization in Plane Elasticity Using Load Path Function Method
AIAA 2016-0233
Aircraft Structural Design I • Monday, 4 January 2016 • 1100 hrs
Preliminary Wing Study of General Aviation Aircraft with PRSEUS panels
AIAA 2016-0234
Aircraft Structural Design I • Monday, 4 January 2016 • 1130 hrs
Bi-Level Optimization of a Conceptual Metallic Wing Box with Stiffness Constraints
AIAA 2016-0235
Aircraft Structural Design I • Monday, 4 January 2016 • 1200 hrs
Minimum Induced Drag Theorems for Multi-Wing Systems
AIAA 2016-0236
Challenges in the Design of Joined Wings • Monday, 4 January 2016 • 0900 hrs
Transonic Aeroelastic Analysis for Multidisciplinary Design Optimization Applications
AIAA 2016-0237
Challenges in the Design of Joined Wings • Monday, 4 January 2016 • 0930 hrs
Aeroelasticity of Joined Wings: Unique Aspects and Challenges
AIAA 2016-0238
Challenges in the Design of Joined Wings • Monday, 4 January 2016 • 1000 hrs
Distributed Optical Sensing in Composite Laminate Adhesive Bonds
AIAA 2016-0239
Challenges in the Design of Joined Wings • Monday, 4 January 2016 • 1030 hrs
Investigating Sub-surface Microstructure in Fiber Reinforced Polymer Composites via X-Ray Tomography Characterization
AIAA 2016-0409
Materials Testing & Characterization I • Monday, 4 January 2016 • 1400 hrs
Interpreting High Temperature Deformation Behavior of a Ceramic Matrix Composite via High Energy X-rays and Numerical Simulation
AIAA 2016-0410
Materials Testing & Characterization I • Monday, 4 January 2016 • 1430 hrs
Computationally Intelligent Image Processing Techniques for Crack Detection in Structural Components from Imaged Data
AIAA 2016-0411
Materials Testing & Characterization I • Monday, 4 January 2016 • 1500 hrs
Real Time In-Situ Sensing of Damage Evolution in Carbon Nanotube-Polymer Nanocomposites under Impact Loading
AIAA 2016-0412
Materials Testing & Characterization I • Monday, 4 January 2016 • 1530 hrs
Aircraft Tire Spin-Up Wear Analysis through Experimental Testing and Computational Modeling
AIAA 2016-0413
Materials Testing & Characterization I • Monday, 4 January 2016 • 1600 hrs
An Evolutionary Multi-Architecture Multi-Objective Optimization Algorithm for Design Space Exploration
AIAA 2016-0414
Design Space Exploration • Monday, 4 January 2016 • 1400 hrs
A Heuristic Approach to Finding the Preferred Design Variable Parameterization for Optimization
AIAA 2016-0415
Design Space Exploration • Monday, 4 January 2016 • 1430 hrs
Comparison of Adaptive Design Space Exploration Methods Applied to S-Duct CFD Simulation
AIAA 2016-0416
Design Space Exploration • Monday, 4 January 2016 • 1500 hrs
Adaptive Model Refinement in Surrogate-based Multiobjective Optimization
AIAA 2016-0417
Design Space Exploration • Monday, 4 January 2016 • 1530 hrs
Rapid Multi-Objective Aerodynamic Design Using Co-Kriging and Space Mapping
AIAA 2016-0418
Design Space Exploration • Monday, 4 January 2016 • 1600 hrs
Multi-Fidelity Aerodynamic Shape Optimization Using Manifold Mapping
AIAA 2016-0419
Design Space Exploration • Monday, 4 January 2016 • 1630 hrs
Aircraft Wing Optimization based on Computationally Efficient Gradient-Enhanced Ordinary Kriging Metamodel Building
AIAA 2016-0420
Design Space Exploration • Monday, 4 January 2016 • 1700 hrs
Reduced Order Modeling of Turbulent Flows using Sparse Coding
AIAA 2016-0462
Reduced Order Modeling I • Monday, 4 January 2016 • 1400 hrs
Expedient and Parallelizable Sparse Coding Algorithm for Large Datasets
AIAA 2016-0463
Reduced Order Modeling I • Monday, 4 January 2016 • 1430 hrs
Reduced Order Models for Generation of Large, High Speed Aerodynamic Databases with Jet Interactions
AIAA 2016-0464
Reduced Order Modeling I • Monday, 4 January 2016 • 1500 hrs
Efficiency Enhancement of Reduced Order Model using Variable Fidelity Modeling
AIAA 2016-0465
Reduced Order Modeling I • Monday, 4 January 2016 • 1530 hrs
Reduced-Order Modeling of Flow-Induced Vibrations in Bellows Joints of Rocket Propulsion Systems
AIAA 2016-0466
Reduced Order Modeling I • Monday, 4 January 2016 • 1600 hrs
Aeroelastic Response of the ACTE Transition Section
AIAA 2016-0467
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1400 hrs
Dynamic Behavior of Initially-Stressed and Post-Buckled Laminated Composite Beams
AIAA 2016-0468
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1430 hrs
Dynamic Response of Aeroelastically Tailored Composite Wing: Analysis and Experiment
AIAA 2016-0469
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1500 hrs
The Influence of Wing Flexibility on the Stability of a Biomimetic Flapping Wing Micro Air Vehicle in Hover
AIAA 2016-0470
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1530 hrs
Damped Free Vibration Response of An Adhesively Bonded Stiffened Plate with Plate-Strip Stiffeners
AIAA 2016-0471
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1600 hrs
Impact of the Wing Sweep Angle and Rib Orientation on Wing Structural Response for Un-Tapered Wings
AIAA 2016-0472
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1630 hrs
Energy Based Representations of Mechanical Shock for Failure Characterization
AIAA 2016-0473
Dynamic Loads, Response, and Vibration I • Monday, 4 January 2016 • 1700 hrs
Parameterization Framework for Aeroelastic Design Optimization of Bio-Inspired Wing Structural Layout
AIAA 2016-0485
Aircraft Structural Design II • Monday, 4 January 2016 • 1400 hrs
Analysis of Designer / Tailored Linear Aero-Piezo-Viscoelastic Energy Harvesting
AIAA 2016-0486
Aircraft Structural Design II • Monday, 4 January 2016 • 1430 hrs
Design and structural analysis of unique structures under an internal vacuum
AIAA 2016-0487
Aircraft Structural Design II • Monday, 4 January 2016 • 1500 hrs
Effects of Shallow-Angle, Thin-Ply Laminates on the Structural Performace of Composite Wing
AIAA 2016-0488
Aircraft Structural Design II • Monday, 4 January 2016 • 1530 hrs
Optimization, Manufacturing and Testing of a Composite Wing with Maximized Tip Deflection
AIAA 2016-0489
Aircraft Structural Design II • Monday, 4 January 2016 • 1600 hrs
Thermal Response of a Spatially Graded Metal-Ceramic Structural Panel to Non-Uniform Heating in Hypersonic Flow
AIAA 2016-0490
Aircraft Structural Design II • Monday, 4 January 2016 • 1630 hrs
A High-Fidelity Approach to Conceptual Design
AIAA 2016-0578
Design Processes and Tools • Tuesday, 5 January 2016 • 0900 hrs
Thermo-Mechanical Analysis and Design of Threaded Fasteners
AIAA 2016-0579
Design Processes and Tools • Tuesday, 5 January 2016 • 0930 hrs
Sizing Study for a First-Order Feasibility Assessment of a Space Vehicle Applied to Space Transportation
AIAA 2016-0580
Design Processes and Tools • Tuesday, 5 January 2016 • 1000 hrs
Electric Multirotor UAV Propulsion System Sizing for Performance Prediction and Design Optimization
AIAA 2016-0581
Design Processes and Tools • Tuesday, 5 January 2016 • 1030 hrs
The Full-Scale Helicopter Flight Simulator Design and Fabrication at CCSU
AIAA 2016-0582
Design Processes and Tools • Tuesday, 5 January 2016 • 1100 hrs
Ascendancy of Extinction-Reignition on Single-Stage Hybrid Sounding Rocket in View of Fuels
AIAA 2016-0583
Design Processes and Tools • Tuesday, 5 January 2016 • 1130 hrs
Effect of Silane Treated Electrospun SiO2 Nanofibers Interleaving on Mode I Fracture Toughness of Glass Epoxy Composites
AIAA 2016-0663
Materials Testing & Characterization II • Tuesday, 5 January 2016 • 0900 hrs
Acoustic Emission Beamforming for Detecting and Localizing Damage in Composite Materials
AIAA 2016-0664
Materials Testing & Characterization II • Tuesday, 5 January 2016 • 0930 hrs
Experimental Investigation of Laser Machining of Sapphire for High Temperature Pressure Transducers
AIAA 2016-0665
Materials Testing & Characterization II • Tuesday, 5 January 2016 • 1000 hrs
Comparisons between Forced-Response and Hysteretic Energy Damping Assessment Methods
AIAA 2016-0666
Materials Testing & Characterization II • Tuesday, 5 January 2016 • 1030 hrs
Development of creep-dominant creep-fatigue testing for Alloy 617
AIAA 2016-0668
Materials Testing & Characterization II • Tuesday, 5 January 2016 • 1130 hrs
Thermodynamics For Gas Turbine Cycles With Analytic Derivatives in OpenMDAO
AIAA 2016-0669
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 0900 hrs
Fuel Thermal Management System Consideration in Conceptual Design Sizing
AIAA 2016-0670
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 0930 hrs
Aircraft System Effects Including Propulsion and Air Cycle Machine Coupled Interactions
AIAA 2016-0671
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 1000 hrs
Impact of High Energy Pulsed Systems on an Aircraft's Power and Thermal Management System
AIAA 2016-0672
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 1030 hrs
An Aerospace Vehicle Model Including a Cryogenic Thermal Subsystem
AIAA 2016-0673
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 1100 hrs
An Overview of the Optimized Integrated Multidisciplinary Systems Program
AIAA 2016-0674
Propulsion & Thermal Design Considerations • Tuesday, 5 January 2016 • 1130 hrs
Analysis of Damage Assessment of Large Hailstone Ingestion into Advanced High Bypass Propulsion system
AIAA 2016-0705
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 0900 hrs
Reduced Order Geometric Mistuning Models using Principal Component Analysis Approximations
AIAA 2016-0706
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 0930 hrs
The Development of an Active Damping and Stiffness Technique for Turbomachinery using Shape Memory Alloys
AIAA 2016-0707
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 1000 hrs
Evaluation of Fiber Optic Strain Sensors for Applications in Structural Health Monitoring
AIAA 2016-0708
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 1030 hrs
Frequency Domain Statistical Damage Identification Development and Analytical Study
AIAA 2016-0709
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 1100 hrs
Frequency Domain Statistical Damage Identification Applied to an Experimental Composite Plate
AIAA 2016-0710
Turbomachinery / Structural Health Monitoring • Tuesday, 5 January 2016 • 1130 hrs
Model-Predictive Control of Flexible Aircraft Dynamics using Nonlinear Reduced-Order Models
AIAA 2016-0711
Dynamics, Feedback Control, and Aeroservoelasticity I • Tuesday, 5 January 2016 • 0900 hrs
Optimal Selection of Control Surfaces for Active Aeroelastic Control of Prescribed Modes
AIAA 2016-0712
Dynamics, Feedback Control, and Aeroservoelasticity I • Tuesday, 5 January 2016 • 0930 hrs
Inverse Dynamics for Deceleration Control of Deployment of Linked Panel Structure in Space
AIAA 2016-0713
Dynamics, Feedback Control, and Aeroservoelasticity I • Tuesday, 5 January 2016 • 1000 hrs
Feedback control of integrally actuated membrane wings: a computational study
AIAA 2016-0714
Dynamics, Feedback Control, and Aeroservoelasticity I • Tuesday, 5 January 2016 • 1030 hrs
Active Piezoelectric Actuation and Control of Highly Flexible Multifunctional Wings
AIAA 2016-0715
Dynamics, Feedback Control, and Aeroservoelasticity I • Tuesday, 5 January 2016 • 1100 hrs
Assessment of Multiscale Design System for Fatigue Life Prediction of Advanced Composite Aircraft Structures
AIAA 2016-0722
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 0900 hrs
Fatigue Damage Prediction in Quasi-Isotropic Open-Hole Tension Coupon using the Kinetic Theory of Fracture
AIAA 2016-0723
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 0930 hrs
3D delamination profile reconstruction for composite laminates using inverse heat conduction
AIAA 2016-0724
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 1000 hrs
Assessment of Composite Damage Growth Tools for Aircraft Structure Part II
AIAA 2016-0725
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 1030 hrs
Progressive Failure Simulation in Laminated Composites under Fatigue Loading by Using Discrete Damage Modeling
AIAA 2016-0726
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 1100 hrs
A Continuum Damage and Discrete Crack Approach for Fatigue Damage Prediction of Laminated Composites
AIAA 2016-0727
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 1130 hrs
A Micromechanical Approach to Low Cycle Fatigue Analysis and Life Prediction of Heterogeneous Materials
AIAA 2016-0728
Special Session: USAF Benchmarking of Composite Fatigue Prediction Methods • Tuesday, 5 January 2016 • 1200 hrs
Micro-Scale Crack Propagation Using the eXtended Finite Element Method
AIAA 2016-0729
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 0900 hrs
The EST Model for Predicting Progressive Damage and Failure of Open Hole Bending Specimens
AIAA 2016-0730
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 0930 hrs
Effect of Strength Variation Along a Single Fiber on Micro-Scale Damage Development in UD-FRPs
AIAA 2016-0731
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 1000 hrs
A Comparative Study of Local and Nonlocal Domain Integration for XFEM Based Stress Intensity Factor Extraction for Fatigue Life Prediction
AIAA 2016-0732
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 1030 hrs
Best Paper
Effect of Notch on the Failure Response of Oxide/Oxide Ceramic Composites
AIAA 2016-0733
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 1100 hrs
In situ study of static and dynamic strain energy density at notch roots and fatigue cracks using digital image correlation
AIAA 2016-0734
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 1130 hrs
A Selectively Activated Continuum-Coupled Extrinsic Cohesive Model
AIAA 2016-0735
Failure Analysis and Prediction I • Tuesday, 5 January 2016 • 1200 hrs
Framework for Probabilistic Analysis of Future Energy Technologies: Hybrid-Electric Propulsion
AIAA 2016-0823
Innovative Designs in Aerospace / Design Education • Tuesday, 5 January 2016 • 1400 hrs
Design of an Automated On-Demand Meal Delivery System Under Emerging and Evolving Passenger Requirements
AIAA 2016-0824
Innovative Designs in Aerospace / Design Education • Tuesday, 5 January 2016 • 1430 hrs
Extending Low-Cost Linux Computers for Education and Applications in Embedded Control and Robotics
AIAA 2016-0825
Innovative Designs in Aerospace / Design Education • Tuesday, 5 January 2016 • 1500 hrs
A Beagle Bone Black Baed AHRS for Control of Small UAS and Small Sounding Rockets
AIAA 2016-0826
Innovative Designs in Aerospace / Design Education • Tuesday, 5 January 2016 • 1530 hrs
AREND: A Sensor Aircraft to support Wildlife Rangers
AIAA 2016-0827
Innovative Designs in Aerospace / Design Education • Tuesday, 5 January 2016 • 1600 hrs
Improved Pre-Strain Method for Generating Goodman Data with Vibration-Based Fatigue Testing
AIAA 2016-0925
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1400 hrs
Experimental, numerical, and analytical free vibration analyses of open-hole composite plates
AIAA 2016-0926
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1430 hrs
A Micromechanical Approach to High Cycle Fatigue Analysis and Life Prediction of Heterogeneous Materials
AIAA 2016-0927
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1500 hrs
A novel crack growth equation based on crack tip opening displacement variation
AIAA 2016-0928
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1530 hrs
Anisotropic Fatigue Crack Growth in High-Strength Aluminium Alloys
AIAA 2016-0929
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1600 hrs
An equivalent crack growth model for creep fatigue life prediction of metals
AIAA 2016-0930
Fatigue & Fracture II • Tuesday, 5 January 2016 • 1630 hrs
Effect of Suspended Particle Shapes on Shear Thickening Fluid Behavior
AIAA 2016-0931
Nanostructured Materials II • Tuesday, 5 January 2016 • 1400 hrs
Grains size and rigid rotations effects on the dynamics and pull-in instability of electrostatically-actuated beams
AIAA 2016-0933
Nanostructured Materials II • Tuesday, 5 January 2016 • 1500 hrs
Effects of POSS Addition on Bisphenol-E Cyanate Ester Network
AIAA 2016-0934
Nanostructured Materials II • Tuesday, 5 January 2016 • 1530 hrs
Modeling of strain gradient-based nanoparticle composite plates with surface elasticity
AIAA 2016-0935
Nanostructured Materials II • Tuesday, 5 January 2016 • 1600 hrs
Best Paper
A Coupled Electromechanical Peridynamics Framework for Modeling Carbon Nanotube Reinforced Polymer Composites
AIAA 2016-0936
Nanostructured Materials II • Tuesday, 5 January 2016 • 1630 hrs
Experimental Characterization and Computational Analysis of Mode I Fracture Toughness of a Nano-Cellulose Z-Pin Reinforced Carbon Fiber Laminate
AIAA 2016-0937
Nanostructured Materials II • Tuesday, 5 January 2016 • 1700 hrs
Multi-scale Topology Optimization
AIAA 2016-0938
Topology Methods and Applications • Tuesday, 5 January 2016 • 1400 hrs
Large-Scale Compliance-Minimization and Buckling Topology Optimization of the Undeformed Common Research Model Wing
AIAA 2016-0939
Topology Methods and Applications • Tuesday, 5 January 2016 • 1430 hrs
A New Topology Optimization Method for Simultaneous Design of Component Layout and Frame Structure of Aircraft Wing
AIAA 2016-0940
Topology Methods and Applications • Tuesday, 5 January 2016 • 1500 hrs
Experimental Validation of Structures Optimised for Frequency Constraints and Dynamic Loading
AIAA 2016-0941
Topology Methods and Applications • Tuesday, 5 January 2016 • 1530 hrs
On a Bio-Inspired Design Methodology for the Simultaneous Topology, Shape, Sizing and Subsystem Placement Optimization of Aircrafts
AIAA 2016-0942
Topology Methods and Applications • Tuesday, 5 January 2016 • 1600 hrs
Combined mesh and penalization adaptivity based topology optimization
AIAA 2016-0943
Topology Methods and Applications • Tuesday, 5 January 2016 • 1630 hrs
Fatigue Analysis of Notched Laminates: A Time-Efficient Macro-Mechanical Approach
AIAA 2016-0977
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1400 hrs
Fatigue Validation of Composite Open Hole Analysis Technique for Standard and Nonstandard Laminate - Part 2
AIAA 2016-0978
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1430 hrs
Fatigue Life Prediction of IM7/977-3 Composite Laminates with Multispatial/Multitemporal Homogenization
AIAA 2016-0979
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1500 hrs
Three-Dimensional Delamination Analysis in Composite Open Hole Tensile Specimens with Cohesive Zone Method
AIAA 2016-0980
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1530 hrs
Interlaminar Fatigue Growth for Fail-Safe Life Limit Analysis
AIAA 2016-0981
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1600 hrs
Fatigue Life of Postbuckled Structures with Indentation Damage
AIAA 2016-0982
Composite Fatigue Damage Prediction Methods • Tuesday, 5 January 2016 • 1630 hrs
Micro Damage Initiation of Isotropic and Composites Structures Using Strain Invariant Failure Theory
AIAA 2016-0983
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1400 hrs
A Residual Strength Prediction Methodology for Composite Laminates Wth Surface Damage Under Tensile Loading
AIAA 2016-0984
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1430 hrs
Probabilistic First Ply Failure Analysis of Wind Turbine Blade Laminates
AIAA 2016-0985
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1500 hrs
Thermal Ablation in Fiber-Reinforced Composite Laminates Subjected to Continuing Lightning Current
AIAA 2016-0986
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1530 hrs
Development of a Combined Cohesive and Extended Finite Element Method to Predict Delamination in Composite Structures
AIAA 2016-0987
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1600 hrs
Predicting Composite Fatigue Life of Wind Turbine Blades Using Constituent-Level Physics and Realistic Aerodynamic Load
AIAA 2016-0988
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1630 hrs
A Beam Theory for Progressively Elastic Damage in Fiber-Reinforced Composite Structures
AIAA 2016-0989
Failure Analysis and Prediction II • Tuesday, 5 January 2016 • 1700 hrs
Material Design Using a NURBS-based Shape Optimization
AIAA 2016-1170
Integrated Computational Materials Engineering (ICME) • Wednesday, 6 January 2016 • 0900 hrs
Development of a Structural Finite Element Progressive Failure Simulation and Integration into the ICM2 Framework
AIAA 2016-1171
Integrated Computational Materials Engineering (ICME) • Wednesday, 6 January 2016 • 0930 hrs
Modeling of Shock Wave Propagation through Energetic Solid State Composites using a Taylor-Galerkin Scheme
AIAA 2016-1172
Integrated Computational Materials Engineering (ICME) • Wednesday, 6 January 2016 • 1000 hrs
Multi-Functional Topology Optimization of Nanocomposite Beams
AIAA 2016-1173
Integrated Computational Materials Engineering (ICME) • Wednesday, 6 January 2016 • 1030 hrs
Information Management Workflow and Tools Enabling Multiscale Modeling Within ICME Paradigm
AIAA 2016-1174
Integrated Computational Materials Engineering (ICME) • Wednesday, 6 January 2016 • 1100 hrs
Development of a High-Fidelity Time-Dependent Aero-Structural Capability for Analysis and Design
AIAA 2016-1175
Aeroelastic Sensitivity Analysis & Applications • Wednesday, 6 January 2016 • 0900 hrs
Adjoint Based Structure and Shape Optimization with Flutter Constraints
AIAA 2016-1176
Aeroelastic Sensitivity Analysis & Applications • Wednesday, 6 January 2016 • 0930 hrs
Continuum Sensitivity Analysis for Aeroelastic Shape Optimization
AIAA 2016-1177
Aeroelastic Sensitivity Analysis & Applications • Wednesday, 6 January 2016 • 1000 hrs
Gradient Based Optimization using Spectral Formulation-Based FSI and Coupled Sensitivity Analysis
AIAA 2016-1178
Aeroelastic Sensitivity Analysis & Applications • Wednesday, 6 January 2016 • 1030 hrs
High-fidelity Aerostructural Optimization of a High Aspect Ratio Tow-steered Wing
AIAA 2016-1179
Aeroelastic Sensitivity Analysis & Applications • Wednesday, 6 January 2016 • 1100 hrs
Model Order Reduction of Aeroservoelastic Model of Flexible Aircraft
AIAA 2016-1222
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 0900 hrs
Optimal manoeuvres with very flexible wings
AIAA 2016-1223
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 0930 hrs
Alternative Unsteady Aerodynamic Uncertainty Modeling Approaches for Aeroservoelastic Reliability Analysis
AIAA 2016-1224
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 1000 hrs
Nonlinear Passive Control Strategies for Suppression of Transonic Flutter
AIAA 2016-1225
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 1030 hrs
Aeroelastic responses identification of a high-aspect-ratio flexible wing model and its active flutter suppression strategy
AIAA 2016-1226
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 1100 hrs
Active Flutter Suppression Combining the Receptance Method and Flutter Margin
AIAA 2016-1227
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 1130 hrs
Active Vibration Control Applications for Adaptive Aircraft Wings Modelled as Thin-Walled Composite Beams
AIAA 2016-1228
Dynamics, Feedback Control, and Aeroservoelasticity II • Wednesday, 6 January 2016 • 1200 hrs
Role of FEA, Closed-Form, and Empirical Models in Certifying Aircraft Composite Structures
AIAA 2016-1232
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 0900 hrs
Extension of Automated 3D Digital Reconstruction to Multi-Directional Fiber Reinforced Composite Microstructures
AIAA 2016-1233
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 0930 hrs
Determining Effective Interface Fracture Properties of 3D Fiber Reinforced Foam Core Sandwich Structures
AIAA 2016-1234
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 1000 hrs
Approach of Interlaminar Characterization for Thick Aircraft Composite Structures
AIAA 2016-1235
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 1030 hrs
Impact Response of Woven Composites with Interlaminar Reinforcement
AIAA 2016-1236
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 1100 hrs
Hybrid Textile Composites as Potential Cryogenic Tank Materials
AIAA 2016-1237
Design, Test and Analysis of Composite Structures I • Wednesday, 6 January 2016 • 1130 hrs
An Open Source Reverse Engineering Workflow: Geometry to Optimization
AIAA 2016-1238
Other Topics in Structures • Wednesday, 6 January 2016 • 0900 hrs
The Effects of Reducing the Structural Mass of the Transit Habitat on the Cryogenic Propellant Required for a Human Phobos Mission
AIAA 2016-1239
Other Topics in Structures • Wednesday, 6 January 2016 • 0930 hrs
Simple Test Functions in Meshless Local Petrov-Galerkin Methods
AIAA 2016-1240
Other Topics in Structures • Wednesday, 6 January 2016 • 1000 hrs
Thermally-Driven Morphing with High Temperature Composites
AIAA 2016-1241
Other Topics in Structures • Wednesday, 6 January 2016 • 1030 hrs
Nonlinear Modelling of Axially Deformable Elastica based on Hyperelasticity
AIAA 2016-1242
Other Topics in Structures • Wednesday, 6 January 2016 • 1100 hrs
Crew Compartment Fire Survivability
AIAA 2016-1243
Air and Space Survivability I • Wednesday, 6 January 2016 • 0900 hrs
Characterization of Hydrodynamic Ram Cavity Dynamics to Transient Spray
AIAA 2016-1244
Air and Space Survivability I • Wednesday, 6 January 2016 • 0930 hrs
Composition Characterization of Cavity Consisting of Multiple Fluids
AIAA 2016-1245
Air and Space Survivability I • Wednesday, 6 January 2016 • 1000 hrs
Wing Design Utilizing Topology Optimization and Additive Manufacturing
AIAA 2016-1246
Air and Space Survivability I • Wednesday, 6 January 2016 • 1030 hrs
Topology Optimization and CFD Analysis of a Hypersonic Vehicle Nose Cone
AIAA 2016-1247
Air and Space Survivability I • Wednesday, 6 January 2016 • 1100 hrs
Characterizing Mechanical Properties of Hybrid Alumina Carbon Fiber Composites with Piezospectroscopy
AIAA 2016-1413
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1400 hrs
Development of Advanced Conformal Ablative TPS Fabricated from Rayon- and Pan-Based Carbon Felts
AIAA 2016-1414
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1430 hrs
Flexible Lightweight Adjustable Stiffness Hinge (FLASH) for Advanced Cable Technology
AIAA 2016-1415
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1500 hrs
Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines
AIAA 2016-1416
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1530 hrs
Development of a Novel Self-Healing Polymer with High Temperature Stability
AIAA 2016-1417
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1600 hrs
An Experimental Study into Active Damping Mechanisms in CNT Nanocomposite
AIAA 2016-1418
Advanced Materials and Processing • Wednesday, 6 January 2016 • 1630 hrs
Uncertainty Quantification for Cargo Hold Fires
AIAA 2016-1419
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1400 hrs
Using Multiple Information Sources to Construct Stochastic Databases to Quantify Uncertainty in Certification Maneuvers
AIAA 2016-1420
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1430 hrs
Optimization Under Uncertainty of Parallel Nonlinear Energy Sinks
AIAA 2016-1421
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1500 hrs
Kona: A Parallel Optimization Library for Engineering-Design Problems
AIAA 2016-1422
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1530 hrs
Sensitivity analysis methods for uncertainty budgeting in system design
AIAA 2016-1423
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1600 hrs
A Multi-Disciplinary Study of Future Fuel Efficient Regional Aircraft
AIAA 2016-1424
Design Including Uncertainty & Frameworks • Wednesday, 6 January 2016 • 1630 hrs
Damping of Sandwich Panels via Acoustic Metamaterials
AIAA 2016-1476
Passive Control and Damping • Wednesday, 6 January 2016 • 1400 hrs
Finite Element Modeling of Longitudinal Metastructures for Passive Vibration Suppression
AIAA 2016-1477
Passive Control and Damping • Wednesday, 6 January 2016 • 1430 hrs
Design of Three Parameter Isolator for the RWA Disturbance Considering Flexible Structural Effects
AIAA 2016-1478
Passive Control and Damping • Wednesday, 6 January 2016 • 1500 hrs
Finite Element Modeling of Fluidic Flexible Matrix Composite (F2MC) Treatments for Bending and Torsional Vibration Control
AIAA 2016-1479
Passive Control and Damping • Wednesday, 6 January 2016 • 1530 hrs
Cellular Lattices with an Internal Topology for High Stiffness and Damping
AIAA 2016-1480
Passive Control and Damping • Wednesday, 6 January 2016 • 1600 hrs
Structural dynamics analysis and passive control of wind turbine vibrations with Tuned Mass Damper (TMD) technique
AIAA 2016-1481
Passive Control and Damping • Wednesday, 6 January 2016 • 1630 hrs
Interfacial Micromechanics and Load Transfer of Off-Aligned Nanocomposites
AIAA 2016-1482
Passive Control and Damping • Wednesday, 6 January 2016 • 1700 hrs
Probabilistic Gust Loads Analysis Accounting for Aeroservoelastic System Uncertainty
AIAA 2016-1483
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1400 hrs
Gust Reconstruction from Flight Data Recording via Numerical Optimisation
AIAA 2016-1484
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1430 hrs
Reduced Order Gust Response Simulation using Computational Fluid Dynamics
AIAA 2016-1485
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1500 hrs
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field
AIAA 2016-1486
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1530 hrs
Adaptive Finite Element in Time Method for Rotorcraft Analysis Using Element Size Control
AIAA 2016-1487
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1600 hrs
Derived Gust Velocities Extracted from Flight Data for Various Aircraft
AIAA 2016-1488
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1630 hrs
Examination of Methods to Separate Gust and Maneuver Load Factors
AIAA 2016-1489
Gust Loads, Response, and Control • Wednesday, 6 January 2016 • 1700 hrs
Ultra-Flexible Advanced Stiffness Truss (U-FAST) for Large Solar Arrays
AIAA 2016-1496
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1400 hrs
Optimization of a Composite Lattice Satellite Central Cylinder Structure Using an Efficient Semi-automated Approach
AIAA 2016-1497
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1430 hrs
Imperfection Insensitivity Analyses of Advanced Composite Tow-Steered Shells
AIAA 2016-1498
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1500 hrs
Modeling the Bistability of Laminated Composite Toroidal Slit Tubes
AIAA 2016-1499
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1530 hrs
Vibrational Analysis of Unitized Curvilinearly Stiffened Composite Panels Subjected to In-plane Loads
AIAA 2016-1500
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1600 hrs
Adhesive-Bonded Shape Memory Alloy Strip Joint for Composite Fan Blade Shape Changing Concept
AIAA 2016-1501
Design, Test and Analysis of Composite Structures II • Wednesday, 6 January 2016 • 1630 hrs
Analytical and Experimental Studies on Delamination Arrest in Bolted-Bonded Composite Structures
AIAA 2016-1502
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1400 hrs
Delamination Growth of Redundantly Joined Sandwich Composites Under Compression
AIAA 2016-1503
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1430 hrs
Sensitivity Analysis of Composite Patch Design Parameters under Low Velocity Impact Loading Conditions
AIAA 2016-1504
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1500 hrs
Finite Element Analysis and Testing of Countersunk Composite Bolted Joints in Double Lap Shear
AIAA 2016-1505
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1530 hrs
A Method for Predicting Fastener Hole Elongation in Composite Joints due to Cyclic Loading
AIAA 2016-1506
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1600 hrs
High Fidelity Bearing and Bypass Response and Failure Prediction of Composite Bolted Joints
AIAA 2016-1507
Structural Joints and Repairs • Wednesday, 6 January 2016 • 1630 hrs
Multiscale Simulation of Reacting Shock Physics
AIAA 2016-1508
Air and Space Survivability II • Wednesday, 6 January 2016 • 1400 hrs
Topology Optimization of a Penetrating Warhead
AIAA 2016-1509
Air and Space Survivability II • Wednesday, 6 January 2016 • 1430 hrs
Dynamic Properties of Additively Manufactured 15-5 Stainless Steel and Three-Dimensional Microstructure Characterization
AIAA 2016-1510
Air and Space Survivability II • Wednesday, 6 January 2016 • 1500 hrs
On the impact tolerance of tensegrity-based planetary landers
AIAA 2016-1511
Air and Space Survivability II • Wednesday, 6 January 2016 • 1530 hrs
Surface Roughness of Electron Beam Melting Ti-6Al-4v Effect on Ultrasonic Testing
AIAA 2016-1512
Air and Space Survivability II • Wednesday, 6 January 2016 • 1600 hrs
Cathodic Protection Tests for the Galvanic Corrosion of Airframe Grade CFRP/Al Systems
AIAA 2016-1654
Materials & Design for Additive Manufacturing • Thursday, 7 January 2016 • 0900 hrs
Fire-Retardant Polyamide 11 Nanocomposites/Elastomer Blends for Selective Laser Sintering: Further Studies
AIAA 2016-1655
Materials & Design for Additive Manufacturing • Thursday, 7 January 2016 • 0930 hrs
On the Fatigue Performance of Additively Manufactured Ti-6Al-4V to Enable Rapid Qualification for Aerospace Applications
AIAA 2016-1656
Materials & Design for Additive Manufacturing • Thursday, 7 January 2016 • 1000 hrs
Powder Bed Models - Numerical Assessment of As-Built Quality
AIAA 2016-1657
Materials & Design for Additive Manufacturing • Thursday, 7 January 2016 • 1030 hrs
Data-Driven Certification of Additively Manufactured Parts
AIAA 2016-1658
Materials & Design for Additive Manufacturing • Thursday, 7 January 2016 • 1100 hrs
An EGO-like Optimization Framework for Simultaneous Aircraft Design and Airline Allocation
AIAA 2016-1659
Mission Driven Design • Thursday, 7 January 2016 • 0900 hrs
Wing Aerostructural Optimization under Uncertain Payload Weight and Aircraft Range
AIAA 2016-1660
Mission Driven Design • Thursday, 7 January 2016 • 0930 hrs
An Aircraft Development Methodology Aligning Design and Strategy to Support Key Decision Making
AIAA 2016-1661
Mission Driven Design • Thursday, 7 January 2016 • 1000 hrs
Allocation-mission-design optimization of next-generation aircraft using a parallel computational framework
AIAA 2016-1662
Mission Driven Design • Thursday, 7 January 2016 • 1030 hrs
Waverider Design, Analysis and Performance Evaluation
AIAA 2016-1663
Mission Driven Design • Thursday, 7 January 2016 • 1100 hrs
Using Complex Variables to Estimate the Derivatives of Nonlinear Reduced-Order Models
AIAA 2016-1707
Reduced Order Modeling II • Thursday, 7 January 2016 • 0900 hrs
Large Deformation Modeling of a Beam Type Structure and a 3D Wingbox using an Enhanced Modal Approach
AIAA 2016-1708
Reduced Order Modeling II • Thursday, 7 January 2016 • 0930 hrs
Optimum Thermal Modes for Coupled Structural-Thermal Reduced Order Models
AIAA 2016-1709
Reduced Order Modeling II • Thursday, 7 January 2016 • 1000 hrs
Modeling Fatigue Crack Propagation in a Ti-Alloy at Elevated Temperature within a Reduced-OrderModel Framework
AIAA 2016-1710
Reduced Order Modeling II • Thursday, 7 January 2016 • 1030 hrs
Geometrically Non-linear Structural Dynamics using Increased-Order Modelling
AIAA 2016-1711
Reduced Order Modeling II • Thursday, 7 January 2016 • 1100 hrs
The Ultimate Factor of Safety for Aircraft and Spacecraft - Its History, Applications and Misconceptions
AIAA 2016-1715
Spacecraft Structural Design • Thursday, 7 January 2016 • 0900 hrs
Thermo-structural design of the Hexafly-INT Experimental Flight Test Vehicle (EFTV) and Experimental Service Module (ESM)
AIAA 2016-1716
Spacecraft Structural Design • Thursday, 7 January 2016 • 0930 hrs
Post-buckling Analysis of Curved Honeycomb Sandwhich Panels Containing Interfacial Disbonds
AIAA 2016-1717
Spacecraft Structural Design • Thursday, 7 January 2016 • 1000 hrs
Integrated Composite Stiffener Structure (ICoSS) Concept for Planetary Entry Vehicles
AIAA 2016-1718
Spacecraft Structural Design • Thursday, 7 January 2016 • 1030 hrs
Forward Skirt Structural Testing on the Space Launch System (SLS) Program
AIAA 2016-1719
Spacecraft Structural Design • Thursday, 7 January 2016 • 1100 hrs
Flutter Analysis of Laminated Curvilinear-Stiffened Plates
AIAA 2016-1720
Spacecraft Structural Design • Thursday, 7 January 2016 • 1130 hrs
Peridynamic Truss Element for Viscoelastic Deformation
AIAA 2016-1721
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 0900 hrs
Bond-Based Peridynamics with an Arbitrary Poisson’s Ratio
AIAA 2016-1722
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 0930 hrs
Peridynamics for Predicting Tensile and Compressive Strength of Notched Composites
AIAA 2016-1723
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 1000 hrs
Mean Stress Effects in Strain Energy-based Criterion for Fatigue Life Prediction
AIAA 2016-1724
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 1030 hrs
Fiber Path Optimization of a Symmetric Laminate with a Cutout for Thermal Buckling, Using a Novel Finite Element Algorithm
AIAA 2016-1725
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 1100 hrs
Influence of microstructure arrangement on the responses of composites beyond one representative unit cel
AIAA 2016-1726
Buckling, Fatigue, and Fracture of Structures I • Thursday, 7 January 2016 • 1130 hrs
A Scalable Adjoint Method for Coupled Flexible Multibody Dynamics
AIAA 2016-1907
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1400 hrs
Shape Optimization of Two-Dimensional Acoustic Metamaterials and Phononic Crystals with a Time-Dependent Adjoint Formulation
AIAA 2016-1908
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1430 hrs
Implementation of discrete adjoint method for parameter sensitivity analysis in chemically reacting flows
AIAA 2016-1909
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1500 hrs
Time-dependent Aero-acoustic Adjoint-based Shape Optimization of Helicopter Rotors in Forward Flight
AIAA 2016-1910
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1530 hrs
Trajectory Optimization Procedure for Interplanetary Transfers based on Direct Collocation Method
AIAA 2016-1911
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1600 hrs
Multi-parametric high-order flow sensitivity analysis
AIAA 2016-1912
Sensitivity Derivations & Optimization Applications • Thursday, 7 January 2016 • 1630 hrs
Identification of Nonlinear Aeroelastic Behavior of a Wing with Pitching and Plunging Freeplay via Higher-Order Spectra Analysis
AIAA 2016-1953
System ID • Thursday, 7 January 2016 • 1400 hrs
Dynamic Beam Solutions for Real-Time Simulation and Control Development of Flexible Rockets
AIAA 2016-1954
System ID • Thursday, 7 January 2016 • 1430 hrs
Flight Shape Estimation of Very Flexible Unmanned Aerial Vehicle
AIAA 2016-1955
System ID • Thursday, 7 January 2016 • 1500 hrs
Efficient Clustering Algorithm Using Modal Assurance Criterion for System Identification
AIAA 2016-1956
System ID • Thursday, 7 January 2016 • 1530 hrs
Operational Modal Analysis of a Rotating Cantilever Beam Using High-Speed Digital Image Correlation
AIAA 2016-1957
System ID • Thursday, 7 January 2016 • 1600 hrs
Modeling of Artificial Hair Sensors for Vibration Control of Flexible Wings
AIAA 2016-1958
System ID • Thursday, 7 January 2016 • 1630 hrs
Classical aeroelastic stability analysis of large composite wind turbine blades
AIAA 2016-1959
Flutter • Thursday, 7 January 2016 • 1400 hrs
Wind Tunnel Flutter Testing of a Highly Swept All-Movable Wing with a Control Surface
AIAA 2016-1960
Flutter • Thursday, 7 January 2016 • 1430 hrs
Development and Wind Tunnel Test of W-WING Whirl Flutter Aeroelastic Demonstrator
AIAA 2016-1961
Flutter • Thursday, 7 January 2016 • 1500 hrs
Time to Flutter of a Maneuvering Viscoelastic Goland Wing
AIAA 2016-1962
Flutter • Thursday, 7 January 2016 • 1530 hrs
Uncertainties in vibratory mode shapes and their effect on flutter speeds
AIAA 2016-1963
Flutter • Thursday, 7 January 2016 • 1600 hrs
Optimization of High Altitude Long Endurance (HALE) Vehicle Subject to Flutter Speed Constraint
AIAA 2016-1964
Flutter • Thursday, 7 January 2016 • 1630 hrs
Experimental investigation of an airfoil response under stall-induced pitching oscillations
AIAA 2016-1965
Flutter • Thursday, 7 January 2016 • 1700 hrs
Aeroelastic Tailoring of Blended Composite Structures using Lamination Parameters
AIAA 2016-1966
Composite Laminate Optimization • Thursday, 7 January 2016 • 1400 hrs
Gradient-Based Optimization of Postbuckled, Steered-Fiber Aircraft Shell Using Equivalent Static Loads
AIAA 2016-1967
Composite Laminate Optimization • Thursday, 7 January 2016 • 1430 hrs
Damping Optimization of Symmetrically Laminated Plates with Shear Deformation using Lamination Parameters
AIAA 2016-1968
Composite Laminate Optimization • Thursday, 7 January 2016 • 1500 hrs
Stacking sequence constraints in non-conventional composite laminate optimisation
AIAA 2016-1969
Composite Laminate Optimization • Thursday, 7 January 2016 • 1530 hrs
Optimization of variable stiffness composite plates with cut-outs subjected to compression, tension and shear using an adjoint formulation
AIAA 2016-1970
Composite Laminate Optimization • Thursday, 7 January 2016 • 1600 hrs
A Discontinuous Shell Element for the Delamination Analysis of Composite Laminates
AIAA 2016-1971
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1400 hrs
Buckling Considerations in the Design of Monolithic Machined Aluminum Structures
AIAA 2016-1972
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1430 hrs
Efficient and robust shell design of space launcher vehicle structures
AIAA 2016-1973
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1500 hrs
Post-Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures
AIAA 2016-1974
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1530 hrs
Vibration and Buckling of Quadrilateral Variable Stiffness Laminated Composite Plates
AIAA 2016-1975
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1600 hrs
Parametric Study of Stiffener Variables on Post-Buckling Response of Frame-Stiffened Composite Panels
AIAA 2016-1976
Buckling, Fatigue, and Fracture of Structures II • Thursday, 7 January 2016 • 1630 hrs
Substructure Versus Property-Level Dispersed Modes Calculation
AIAA 2016-2170
Dynamic Loads, Response, and Vibration II • Friday, 8 January 2016 • 0900 hrs
Acoustic Analysis of A Partially Open Spacecraft Cavity using Multi-Domain Boundary Element Method
AIAA 2016-2171
Dynamic Loads, Response, and Vibration II • Friday, 8 January 2016 • 0930 hrs
Assessing Sine and Random Stresses and Fatigue Life
AIAA 2016-2172
Dynamic Loads, Response, and Vibration II • Friday, 8 January 2016 • 1000 hrs
Non-Stationary Random Vibration Analysis Using Multi-Correlated Random Processes Excitations
AIAA 2016-2173
Dynamic Loads, Response, and Vibration II • Friday, 8 January 2016 • 1030 hrs
Exploring Entropy for Continuous Systems
AIAA 2016-2174
Dynamic Loads, Response, and Vibration II • Friday, 8 January 2016 • 1100 hrs
Testing of a Stitched Composite Large-Scale Pressure Box
AIAA 2016-2175
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 0900 hrs
Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part I: Ultimate Design Loads
AIAA 2016-2176
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 0930 hrs
Testing and Analysis of a Composite Non-Cylindrical Aircraft Fuselage Structure, Part II: Severe Damage
AIAA 2016-2177
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 1000 hrs
Imparting Barely Visible Impact Damage to a Stitched Composite Large-Scale Pressure Box
AIAA 2016-2178
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 1030 hrs
Compressive Loading and Modeling of Stitched Composite Stiffeners
AIAA 2016-2179
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 1100 hrs
Tension and Bending Testing of an Integral T-cap for Stitched Composite Airframe Joints
AIAA 2016-2180
Special Session: Stiffened, Stitched Composite Structures • Friday, 8 January 2016 • 1130 hrs
Low Velocity Impact Test and Analysis of Laminated Structures
AIAA 2016-2181
Impact Damage in Composites • Friday, 8 January 2016 • 0900 hrs
Modeling Axial Impact Response of Sandwich Panels using Probability-Based Finite Element Analysis
AIAA 2016-2182
Impact Damage in Composites • Friday, 8 January 2016 • 0930 hrs
Correlating Impact, Micro CT Inspection, and Residual Strength of Carbon/Epoxy Rods
AIAA 2016-2183
Impact Damage in Composites • Friday, 8 January 2016 • 1000 hrs
Prediction of Low-Velocity Face-on Impact Response of Composite Laminates using High-Fidelity Finite Element Modeling Techniques
AIAA 2016-2184
Impact Damage in Composites • Friday, 8 January 2016 • 1030 hrs