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A theory for base pressures on multinozzle rocket configurationsTurbulent base flowfields in multinozzle configurations, considering adiabatic flow and determining base pressure distribution from reverse jet impingement
Document ID
19700052395
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Abbud, K. A.
Lamb, J. P.
Lenzo, C. S.
Date Acquired
August 5, 2013
Publication Date
April 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 69-570
Report Number: AIAA PAPER 69-570
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY
Location: COLORADO SPRINGS, CO
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A28511
Funding Number(s)
CONTRACT_GRANT: NAS8-20321
Distribution Limits
Public
Copyright
Other

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