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A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Document ID
19660010454
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Mitcham, G. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 27, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L56K19
Accession Number
66N19743
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FIGHTER AIRCRAFT
STABILITY AND CONTROL
SWEPT WING
LONGITUDINAL CONTROL
LATERAL STABILITY

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