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V/stol plenum chamber combustion research study, phase i final reportV/STOL plenum chamber design for combustion system efficiency in fan duct of turbofan engine
Document ID
19650015373
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maggitti, L. (Naval Air Engineering Center Philadelphia, PA, United States)
Date Acquired
August 2, 2013
Publication Date
April 28, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-63093
NAEC-AEL-1797
Report Number: NASA-CR-63093
Report Number: NAEC-AEL-1797
Accession Number
65N24974
Funding Number(s)
CONTRACT_GRANT: NASA ORDER 121
CONTRACT_GRANT: NASA ORDER 121
CONTRACT_GRANT: NASA ORDER R-121
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
V/STOL AIRCRAFT
PLENUM CHAMBER
TURBOFAN ENGINE

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