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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
19660054363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ericsson, L. E.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 66-471
Report Number: AIAA PAPER 66-471
Accession Number
66A33653
Funding Number(s)
CONTRACT_GRANT: NAS8-5338
CONTRACT_GRANT: NAS8-11238
Distribution Limits
Public
Copyright
Other
Keywords
SHOCK WAVE
BOUNDARY LAYER
SLENDER BODY
SUPERSONIC FLOW
FLOW SEPARATION

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