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STRUCTURAL-LOADS SURVEYS ON TWO TILT-WING VTOL CONFIGURATIONSStructural load surveys on tilt-wing vtol aircraft airframe vibratory loads of vz-ii vtol and wing loads of research model in wind tunnel tests
Document ID
19630004830
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ward, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1960
Subject Category
Thermodynamics And Combustion
Accession Number
63N14706
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING LOADING
VTOL AIRCRAFT
WIND TUNNEL STABILITY TEST
VZ-2 AIRCRAFT
VIBRATORY LOADING
AIRFRAME

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