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Evaluation of a bulk calorimeter and heat balance for determination of supersonic combustor efficiencyResults are presented from the shakedown and evaluation test of a bulk calorimeter. The calorimeter is designed to quench the combustion at the exit of a direct-connect, hydrogen fueled, scramjet combustor model, and to provide the measurements necessary to perform an analysis of combustion efficiency. Results indicate that the calorimeter quenches reaction, that reasonable response times are obtained, and that the calculated combustion efficiency is repeatable within + or -3 percent and varies in a regular way with combustor model parameters such as injected fuel equivalence ratio.
Document ID
19810004547
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Mcclinton, C. R.
(NASA Langley Research Center Hampton, VA, United States)
Anderson, G. Y.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
L-13943
NASA-TP-1739
Report Number: L-13943
Report Number: NASA-TP-1739
Accession Number
81N13058
Funding Number(s)
PROJECT: RTOP 505-32-93-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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