Aerodynamic and aerothermodynamic comparisons between flight and ground test for the Space Shuttle at hypersonic speeds are discussed. All of the comparisons are taken from papers published by researchers active in the Space Shuttle program. The aerodynamic comparisons include stability and control derivatives, center-of-pressure location, and reaction control jet interaction. Comparisons are also discussed for various forms of heating, including catalytic, boundary layer, top centerline, side fuselage, OMS pod, wing leading edge, and shock interaction. The jet interaction and center-of-pressure location flight values exceeded not only the predictions but also the uncertainties of the predictions. Predictions were significantly exceeded for the heating caused by the vortex impingement on the OMS pods and for heating caused by the wing leading-edge shock interaction.
Space Shuttle Hypersonic Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results
1993
29 pages
Report
No indication
English
Manned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Aerodynamics , Aerodynamic characteristics , Aerodynamic heating , Aerothermodynamics , Boundary layer transition , Hypersonics , Space shuttle orbiters , Space shuttles , Correlation , Flight control , Flight tests , Ground tests , Hypersonic speed , Jet control , Center of pressure , Fuselages , Impingement , Leading edges , Pods (External stores) , Stability derivatives , Vortices , Wings
AERODYNAMIC AND AEROTHERMODYNAMIC LAYOUT OF THE HYPERSONIC FLIGHT EXPERIMENT - SHEFEX
British Library Conference Proceedings | 2004
|