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Tabulated pressure data for a series of controls on a 60 deg. delta wing at mach numbers of 1.61 and 2.01Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.01
Document ID
19650018846
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Czarnecki, K. R. (NASA Langley Research Center Hampton, VA, United States)
Lord, D. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 30, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L55L05
Accession Number
65N28447
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
PRESSURE DISTRIBUTION

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