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Numerical study of contaminant effects on combustion of hydrogen, ethane, and methane in airA numerical study was performed to assess the effects of vitiated air on the chemical kinetics of hydrogen, ethane, and methane combustion with air. A series of calculations in static reacting systems was performed, where the initial temperature was specified and reactions occurred at constant pressure. Three different types of test flow contaminants were considered: NO, H2O, and a combination of H2O and CO2. These contaminants are present in the test flows of facilities used for hypersonic propulsion testing. The results were computed using a detailed reaction mechanism and are presented in terms of ignition and reaction times. Calculations were made for a wide range of contaminant concentrations, temperatures and pressures. The results indicate a pronounced kinetic effect over a range of temperatures, especially with NO contamination and, to a lesser degree, with H2O contamination. In all cases studied, CO2 remained kinetically inert, but had a thermodynamically effect on results by acting as a third body. The largest effect is observed with combustion using hydrogen fuel, less effect is seen with combustion of ethane, and little effect of contaminants is shown with methane combustion.
Document ID
19950056406
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lai, H. T.
(NYMA, Inc. Brook Park, OH, United States)
Thomas, S. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1995
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 95-6097
Meeting Information
Meeting: AIAA International Aerospace Planes and Hypersonics Technologies Conference
Location: Chattanooga, TN
Country: United States
Start Date: April 3, 1995
End Date: April 7, 1995
Accession Number
95A88005
Distribution Limits
Public
Copyright
Other

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