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Panel flutter aerodynamics Final report, 25 Jun. 1964 - 25 Sep. 1965Flutter boundary for flat panel in low supersonic flow and boundary layer pressure-velocity probe design
Document ID
19660007205
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zeydel, E. F. E. (Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-69144
Report Number: NASA-CR-69144
Accession Number
66N16494
Funding Number(s)
CONTRACT_GRANT: NAS8-11396
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PANEL FLUTTER
BOUNDARY LAYER
SUPERSONIC FLOW
VELOCITY PROBE
PRESSURE PROBE

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