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Further wind tunnel measurements of pressure signatures for a 0.0041-scale model of the space shuttle orbiterPressure signatures for a 0.0041 scale model of the space shuttle orbiter were measured in the wind tunnel at Mach numbers from 1.3 to 4.0. The angles of attack were 0 deg, 10 deg, 20 deg and 30 deg. At each angle of attack the model was rolled from 0 deg to 120 deg in 30 deg increments.
Document ID
19760021100
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mendoza, J. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-73120
A-6533
Report Number: NASA-TM-X-73120
Report Number: A-6533
Accession Number
76N28188
Funding Number(s)
PROJECT: RTOP 506-26-31-06-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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