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Zero lift-drag at mach 1.42, 1.83, and 2.21 of a series of wings with variations of thickness ratio and chordZero lift-drag at supersonic speeds of wings with low thickness ratios
Document ID
19650014089
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Shrout, B. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2811
Report Number: NASA-TN-D-2811
Accession Number
65N23690
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOW ASPECT RATIO WING
THIN WING
ZERO LIFT
SUPERSONIC SPEED

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