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Investigation of the burning configuration of a coaxial injector in a combustion chamberAn analytical investigation was made into the stability of the burning configuration of a single coaxial injector surrounded by similar injectors. The stability criteria was based on an average pressure difference along the boundaries of the adjacent stream tubes as calculated using Spaulding's numerical method. The results indicate qualitatively that there is a tendency for the injectors to have different burning configurations. It is believed that the configuration achieved is random, however once the burning configuration is established, it is believed to persist.
Document ID
19780014205
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ohara, J.
(Texas A&I Univ. Kingsville, TX, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-135383
Report Number: NASA-CR-135383
Accession Number
78N22148
Funding Number(s)
CONTRACT_GRANT: NSG-3112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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