NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Chemical kinetic modeling of propane oxidation behind shock wavesThe stoichiometric combustion of propane behind incident shock waves was studied experimentally and analytically over a temperature range from 1700 K to 2600 K and a pressure range from 1.2 to 1.9 atm. Measurements of the concentrations of carbon monoxide (CO) and carbon dioxide (CO2) and the product of the oxygen atom and carbon dioxide concentrations (O)(CO) were made after passage of the incident shock wave. A kinetic mechanism was developed which, when used in a computer program for a flowing, reacting gas behind an incident shock wave predicted experimentally measured results quite well. Ignition delay times from the literature were also predicted quite well. The kinetic mechanism consisted of 59 individual kinetic steps.
Document ID
19770021307
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mclain, A. G.
(NASA Langley Research Center Hampton, VA, United States)
Jachimowski, C. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
L-11606
NASA-TN-D-8501
Report Number: L-11606
Report Number: NASA-TN-D-8501
Accession Number
77N28251
Funding Number(s)
PROJECT: RTOP 505-03-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available