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Aerodynamics of the model airplane. Part 1 - Airfoil measurementsAirfoil measurements that show behavior of wing sections in low-turbulence stream in Reynolds number range from 20,000 to 170,000
Document ID
19700029685
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schmitz, F. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
RSIC-721-PT-1
NASA-TM-X-60976
Accession Number
70N39001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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