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Free-flight measurements of aerodynamic viscous effects on lifting re-entry 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
19670056089
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Horstman, C. C.
Kussoy, M. I.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 67-165
Report Number: AIAA PAPER 67-165
Accession Number
67A34818
Distribution Limits
Public
Copyright
Other
Keywords
VISCOUS DRAG
REENTRY VEHICLE
FREE FLIGHT
LIFT-DRAG RATIO
SHOCK TUNNEL

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