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Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Document ID
19930083872
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sacks, Alvin H
Date Acquired
August 16, 2013
Publication Date
November 1, 1954
Report/Patent Number
NACA-TN-3283
Accession Number
93R13162
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY, DYNAMIC
WINGS, COMPLETE - THEORY
WING-BODY COMBINATIONS - MISSILES
WING-FUSELAGE COMBINATIONS - AIRPLANES
DAMPING DERIVATIVES - STABILITY
STABILITY, STATIC

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