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Transonic and Supersonic Flutter Trend Investigation of a Variable-sweep WingWind tunnel analysis of flutter trend for variable sweep aircraft at transonic and supersonic speeds
Document ID
19660022440
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goetz, R. C. (NASA Langley Research Center Hampton, VA, United States)
Stonesifer, J. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-598
Report Number: NASA-TM-X-598
Accession Number
66N31730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER ANALYSIS
VARIABLE SWEEP
SUPERSONIC SPEED
TRANSONIC SPEED

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