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INFLUENCE OF AUTOMATIC CONTROL OF ROLL COUPLING AND PITCH-UP ON TAIL LOADSStability & control of aircraft - aerodynamic loading
Document ID
19630008164
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Stone, R. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
June 17, 1957
Subject Category
Auxiliary Systems
Report/Patent Number
NACA-RM-L57D18A
Report Number: NACA-RM-L57D18A
Accession Number
63N18041
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
AUTOMATIC CONTROL
AERODYNAMIC LOAD

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