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Some aspects of gaseous secondary injection with application to thrust vector controlTwo dimensional sonic nonreacting gaseous secondary injection into supersonic primary stream with turbulent boundary layer for application to thrust vector control
Document ID
19710050089
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Doyle, H.
Guhse, R. D.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 71-750
Report Number: AIAA PAPER 71-750
Meeting Information
Meeting: PROPULSION JOINT SPECIALIST CONFERENCE
Location: SALT LAKE CITY, UT
Country: US
Start Date: June 14, 1971
End Date: June 18, 1971
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, SOCIETY OF AUTOMOTIVE ENGINEERS
Accession Number
71A30786
Funding Number(s)
CONTRACT_GRANT: NSG-592
Distribution Limits
Public
Copyright
Other

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