Accession Number : ADA613690


Title :   Prediction of Combustion Instability with Detailed Chemical Kinetics


Descriptive Note : Technical paper Dec 2014-Jan 2015


Corporate Author : AIR FORCE RESEARCH LAB EDWARDS AFB CA AEROSPACE SYSTEMS DIRECTORATE


Personal Author(s) : Sardeshmukh, Swanand V ; Anderson lMatthew E , William E ; Sankaran, Venkateswaran


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a613690.pdf


Report Date : Dec 2014


Pagination or Media Count : 20


Abstract : Combustion instability in an unstable single element rocket chamber using methane as the fuel is computationally studied. Effects of the kinetics mechanism are examined by comparing the results using a single step global mechanism and a detailed mechanism with 32 species and 177 reactions. Significant differences between the two predictions are identified including the amplitude of the unsteady pressure oscillations, and more importantly, the underlying mechanisms responsible for driving the combustion instabilities.


Descriptors :   *COMBUSTION STABILITY , *KINETICS , AMPLITUDE , FUELS , GLOBAL , INSTABILITY , METHANE , PREDICTIONS , REACTION KINETICS


Subject Categories : Combustion and Ignition


Distribution Statement : APPROVED FOR PUBLIC RELEASE