TY - GEN
T1 - Numerical simulation of combustion of unlike impinging jets near a wall
AU - Park, Ki Sun
AU - Sardeshmukh, Swanand V.
AU - Heister, Stephen D.
AU - Sankaran, Venkateswaran
N1 - Publisher Copyright:
© 2013, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2013
Y1 - 2013
N2 - The combustion of gas-gas hypergolic propellants with MMH (Monomethylhydrazine) as fuel and RFNA (Red fuming nitric acid) as oxidizer are studied numerically for unlike impinging jets near an inclined wall using a detailed chemical reaction mechanism. The current study focuses on quantifying the effect of the inclined wall on the ignition characteristics: namely, contact time/location and ignition delay/location. Furthermore, the effect of wall is assessed with respect to mixing and flame spreading. The baseline three-dimensional simulation results compare two domains, with and without the inclined wall, under the same inlet flow conditions. These results show that the space between the wall surface and injector tips acts as a mixing zone with intensified vorticity and heat release rate. Two-dimensional results for various injection velocities are also presented and are compared with the three-dimensional results.
AB - The combustion of gas-gas hypergolic propellants with MMH (Monomethylhydrazine) as fuel and RFNA (Red fuming nitric acid) as oxidizer are studied numerically for unlike impinging jets near an inclined wall using a detailed chemical reaction mechanism. The current study focuses on quantifying the effect of the inclined wall on the ignition characteristics: namely, contact time/location and ignition delay/location. Furthermore, the effect of wall is assessed with respect to mixing and flame spreading. The baseline three-dimensional simulation results compare two domains, with and without the inclined wall, under the same inlet flow conditions. These results show that the space between the wall surface and injector tips acts as a mixing zone with intensified vorticity and heat release rate. Two-dimensional results for various injection velocities are also presented and are compared with the three-dimensional results.
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U2 - 10.2514/6.2013-4156
DO - 10.2514/6.2013-4156
M3 - Conference contribution
AN - SCOPUS:85071652359
SN - 9781624102226
T3 - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
BT - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013
Y2 - 14 July 2013 through 17 July 2013
ER -