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title: 34th AIAA Fluid Dynamics Conference and Exhibit
Aerodynamic Database Development for Mars Smart Lander Vehicle Configurations
Aerodynamic Design of Heavy Vehicles Reporting Period January 15, 2004 through April 15, 2004
Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data
Aeroheating Design Issues for Reusable Launch Vehicles: A Perspective
Aeroheating Design Issues for Reusable Launch Vehicles: A Perspective
Aeronautics Into the Virtual Age
Application of Circulation Control Technology to Airframe Noise Reduction
Assessment of CFD-based Response Surface Model for Ares I Supersonic Ascent Aerodynamics
Axisymmetric computational fluid dynamics analysis of a film/dump-cooled rocket nozzle plume
Boundary Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander
Boundary Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander
Computational Fluid Dynamics-Based Aeroservoelastic Analysis with Hyper-X Applications
DDS-Suite - A Dynamic Data Acquisition, Processing, and Analysis System for Wind Tunnel Testing
Description of a Website Resource for Turbulence Modeling Verification and Validation
Development of a Flexible Framework for Hypersonic Navier-Stoke Space Shuttle Orbiter Meshes
Development of the Dual Aerodynamic Nozzle Model for the NTF Semi-Span Model Support System
Downstream Effects on Orbiter Leeside Flow Separation for Hypersonic Flows