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Chemical kinetic modeling of propane oxidation behind shock waves
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McLain, A. G. Jachimowski, C. J. |
| Copyright Year | 1977 |
| Description | The 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. |
| File Size | 2001808 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770021307 |
| Archival Resource Key | ark:/13960/t7gr1q47w |
| Language | English |
| Publisher Date | 1977-07-01 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Shock Waves Concentration Composition Reaction Kinetics Carbon Dioxide Ignition Oxidation Carbon Monoxide Propane Computer Programs Time Lag Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
