NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygenShear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume analysis
Document ID
19680006379
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Edelman, R. (General Applied Science Labs., Inc. Westbury, NY, United States)
Fortune, O. (General Applied Science Labs., Inc. Westbury, NY, United States)
Date Acquired
August 4, 2013
Publication Date
December 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-61494
GASL-TR-681
Report Number: NASA-CR-61494
Report Number: GASL-TR-681
Accession Number
68N15848
Funding Number(s)
CONTRACT_GRANT: NAS8-21047
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available