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Effects of oblique shock waves in the near field of rocket plumesRocket nozzle originated oblique shock waves effect on near-field plume inpingement flows, heat transfer and pressure distribution
Document ID
19700039305
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lacinski, T. M.
Leng, J.
Osonitsch, C. W.
Date Acquired
August 5, 2013
Publication Date
November 1, 1969
Subject Category
Propulsion Systems
Accession Number
70A15421
Funding Number(s)
CONTRACT_GRANT: NAS9-1100
CONTRACT_GRANT: NAS8-25000
Distribution Limits
Public
Copyright
Other

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