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An experimental investigation of thrust vector control by secondary injectionFlow field produced by secondary gas injection into supersonic primary stream
Document ID
19650023942
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Guhse, R. D. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-297
Report Number: NASA-CR-297
Accession Number
65N33543
Funding Number(s)
CONTRACT_GRANT: NSG-592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SECONDARY INJECTION
FLOW FIELD
SUPERSONIC FLOW

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