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Aeroelastic instability caused by slender payloads.Terminal shock-boundary layer interaction on slender cone-cylinder payloads at supersonic speeds and resulting flow separation
Document ID
19670038484
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ericsson, L. E.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 66-471
Report Number: AIAA PAPER 66-471
Accession Number
67A17213
Funding Number(s)
CONTRACT_GRANT: NAS8-11238
CONTRACT_GRANT: NAS8-5338
Distribution Limits
Public
Copyright
Other
Keywords
FLOW SEPARATION
SUPERSONIC FLOW
BOUNDARY LAYER
SHOCK WAVE
SLENDER BODY

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