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Supercritical oxygen heat transferHeat transfer to supercritical oxygen was experimentally measured in electrical heated tubes. Experimental data were obtained for pressures ranging from 17 to 34.5 MPa (2460 to 5000 psia), and heat fluxes from 2 to 90 million w/sq cm (1.2 to 55 Btu/(sq in. sec)). Bulk temperatures ranged from 96 to 217 K (173 to 391 R). Experimental data obtained by other investigators were added to this to increase the range of pressure down to 2 MPa (290 psia) and increase the range of bulk temperature up to 566 K (1019 R). From this compilation of experimental data a correlating equation was developed which predicts over 95% of the experimental data within + or - 30%.
Document ID
19780009399
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Spencer, R. G.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Rousar, D. C.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-135339
Report Number: NASA-CR-135339
Accession Number
78N17342
Funding Number(s)
CONTRACT_GRANT: NAS3-20384
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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