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Effect of wing loading and altitude on lateral stability and control characteristics of an airplane as determined by tests of a model in the free-flight tunnel
Document ID
19930092562
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Seacord, Charles L , Jr
Date Acquired
September 6, 2013
Publication Date
June 1, 1943
Report/Patent Number
NACA-WR-L-522
NACA-ARR-3F25
Report Number: NACA-WR-L-522
Report Number: NACA-ARR-3F25
Accession Number
93R21852
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY & CONTROL, LATERAL - EFFECT OF ALTITUDE
AILERONS - DEFLECTION
INSTABILITY, SPIRAL
ROLLING
MOMENTS OF INERTIA
STABILITY, DIRECTIONAL
AIRPLANES, FIGHTER
OSCILLATIONS, LATERAL
STABILITY TESTS, WIND-TUNNEL
LOADING, WING

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