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Supersonic aerodynamic characteristics of a lifting-body orbiter model with a blunted delta planform at Mach 2.30 to 4.60An investigation has been made in the Langley Unitary Plan wind tunnel to determine the aerodynamic characteristics of a lifting-body orbiter model with a blunted delta planform. The model was tested at Mach numbers from 2.30 to 4.60, at nominal angles of attack from -4 deg to 60 deg and angles of sideslip from -4 deg to 10 deg, and at a Reynolds number of 2.5 million per foot.
Document ID
19720023341
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blair, A. B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
L-8366
NASA-TM-X-2581
Accession Number
72N30991
Funding Number(s)
PROJECT: RTOP 502-37-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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