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Effects of shock-induced separation Technical summary reportSupersonic and subsonic shock wave boundary layer separation studies on aeroelasticity of Saturn launch vehicles
Document ID
19700006492
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ericsson, L. E. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Guenther, R. A. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Reding, J. P. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
L-87-69-1
NASA-CR-107673
Report Number: L-87-69-1
Report Number: NASA-CR-107673
Accession Number
70N15796
Funding Number(s)
CONTRACT_GRANT: NAS8-20354
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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