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An Airfoil Shape for Efficient Flight at Supercritical Mach NumbersNo abstract available
Document ID
19720066117
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Whitcomb, R. T. (NASA Langley Research Center Hampton, VA, United States)
Clark, L. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1965
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
L-4517
NASA-TM-X-1109
Accession Number
72N73989
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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