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Theoretical and Experimental Studies of Cambered and Twisted Wings Optimized for Flight at Supersonic SpeedsNo abstract available
Document ID
19680067736
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Brown, C. E. (NASA Langley Research Center Hampton, VA, United States)
Klunker, E. B. (NASA Langley Research Center Hampton, VA, United States)
Mc Lean, F. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 4, 2013
Publication Date
January 1, 1960
Subject Category
Aircraft Design, Testing And Performance
Aerodynamics
Aeronautics (General)
Report/Patent Number
NASA-TM-X-60837
Report Number: NASA-TM-X-60837
Accession Number
68N82547
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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