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Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speedsWind tunnel tests to determine lateral-directional stability of aircraft from transonic to supersonic speeds
Document ID
19660010446
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Ball, L. H. (NASA Ames Research Center Moffett Field, CA, United States)
Smith, W. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 4, 1956
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A55J03
Accession Number
66N19735
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
DIRECTIONAL STABILITY
SUPERSONIC SPEED
WIND TUNNEL STABILITY TEST
TRANSONIC SPEED
LATERAL STABILITY

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