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Free-flight measurements of aerodynamic viscous effects on lifting reentry bodies.Lift-drag ratio, lift and drag coefficients and angle of attack effects on Gemini and Apollo reentry vehicles measured in shock tunnel under free flight conditions
Document ID
19670039778
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horstman, C. C.
Kussoy, M. I.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 67-165
Report Number: AIAA PAPER 67-165
Accession Number
67A18507
Distribution Limits
Public
Copyright
Other
Keywords
SHOCK TUNNEL
FREE FLIGHT
LIFT-DRAG RATIO
VISCOUS DRAG
REENTRY VEHICLE

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