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Design of supersonic combustors based on pressure-area fields.Supersonic combustor length and contours for optimum performance determined from one- dimensional pressure-area analysis
Document ID
19670055103
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Billig, F. S.
Date Acquired
August 3, 2013
Publication Date
January 1, 1967
Subject Category
Thermodynamics And Combustion
Accession Number
67A33832
Funding Number(s)
CONTRACT_GRANT: NOW-62-0604-C
CONTRACT_GRANT: NASA ORDER SC-R-76-21-09-001
CONTRACT_GRANT: NSF GP-5734
CONTRACT_GRANT: DA-ARO/D/-31-124-G841
CONTRACT_GRANT: NGR-39-003-005
Distribution Limits
Public
Copyright
Other
Keywords
COMBUSTION EFFICIENCY
COMBUSTOR
SUPERSONIC COMBUSTION
RAMJET ENGINE

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