NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Aerodynamic characteristics of a 55 deg clipped-delta-wing orbiter model at Mach numbers from 1.60 to 4.63Wind tunnel tests to determine the supersonic aerodynamic characteristics of a delta wing space shuttle orbiter model were conducted. The model was tested at Mach numbers from 1.60 to 4.63, at nominal angles of attack from minus 2 degrees to plus 30 degrees, nominal sideslip angles of minus 4 degrees to plus 10 degrees, and Reynolds numbers from 1.8 to 2.5 times one million per foot.
Document ID
19730015331
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blair, A. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Grow, J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Aircraft
Report/Patent Number
L-8732
NASA-TM-X-2748
Report Number: L-8732
Report Number: NASA-TM-X-2748
Accession Number
73N24058
Funding Number(s)
PROJECT: RTOP 502-37-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available