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Experimental Effect of Gas Flow Transients on the Heat Release of Burning Liquid Drops in a Rocket CombustorExperimental effect of gas flow transients on heat emission of burning liquid drops in a rocket combustor
Document ID
19630004075
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Heidmann, M. F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1963
Subject Category
Physics, Solid-State
Report/Patent Number
NASA-TN-D-1576
Report Number: NASA-TN-D-1576
Accession Number
63N13951
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID DROP
ROCKET COMBUSTOR
BURNING RATE
GAS FLOW
THERMAL EMISSION
DROP TEST

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