No AccessIncorporation of Ablative Shape Change into Conceptual Hypersonic Mission DesignHarish Saranathan and Michael J. GrantHarish SaranathanPurdue UniversitySearch for more papers by this author and Michael J. GrantPurdue UniversitySearch for more papers by this authorAIAA 2016-0020Session: Atmospheric Entry, Hypersonic Flight and Aeroassist Technology IPublished Online:1 Jan 2016https://doi.org/10.2514/6.2016-0020SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byIncorporation of Effects of Control Surfaces into Hypersonic Trajectory Optimization FrameworkHarish Saranathan and Michael J. Grant10 June 2016 What's Popular AIAA Atmospheric Flight Mechanics Conference 4-8 January 2016San Diego, California, USAhttps://doi.org/10.2514/6.2016-0020 CrossmarkInformationCopyright © 2016 by Harish Saranathan and Michael J. Grant. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesAerothermodynamicsComputational Fluid DynamicsConservation of Momentum EquationsEquations of Fluid DynamicsFinite Difference MethodFlow RegimesFluid DynamicsFluid Flow PropertiesShock WavesSkin Friction KeywordsPressure CoefficientThermal Protection SystemAngle of AttackTrajectory OptimizationAerodynamic CoefficientsFlow ConditionsWall TemperatureFlight Path AngleEarthHypersonic VehiclesPDF Topics Atmospheric Flight Mechanics