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Test of NACA 21 Airfoil (Modified NACA M-6) Including Characteristics at Positive and Negative Angles of AttackNo abstract available
Document ID
20150012617
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Anderson, Raymond F. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
July 7, 2015
Publication Date
June 25, 1932
Subject Category
Aircraft Design, Testing And Performance
Research And Support Facilities (Air)
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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