TY - GEN
T1 - Numerical simulation of forced ignition of jet-fuel/air using large eddy simulation (LES) and a tabulation-based ignition model
AU - Tang, Yihao
AU - Hassanaly, Malik
AU - Raman, Venkat
AU - Sforzo, Brandon A.
AU - Seitzman, Jerry M.
N1 - Publisher Copyright:
© 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2019
Y1 - 2019
N2 - A comprehensive computational model for forced ignition is used to simulate a canonical experiment for the high-altitude relight process. The focus here is on simulating the ignition probability for a given set of operating conditions. In particular, the effect of fuel composition on the ignition characteristics is studied. Forced ignition using an external igniter involves the interaction of chemical kinetics, turbulent flow, and the uncertainties associated with the igniter energy deposition process. In this work, a detailed model for the growth and stabilization of the hot kernel produced by the igniter is used. Large eddy simulation (LES) is used to describe the turbulent flow and the fuel-air concentration fluctuations, as well as their temporal evolution. Ignition is described as a probabilistic event, with the randomness a result of the uncertainties in turbulent state of the system and the igniter energy deposition. Using an uncertainty quantification approach, the ignition probability is estimated for three different fuels. It is shown that the model correctly reproduces the ignition trends observed in the experiments. Moreover, it is demonstrated that uncertain parameters may be calibrated using related experiments and extended to other operating conditions.
AB - A comprehensive computational model for forced ignition is used to simulate a canonical experiment for the high-altitude relight process. The focus here is on simulating the ignition probability for a given set of operating conditions. In particular, the effect of fuel composition on the ignition characteristics is studied. Forced ignition using an external igniter involves the interaction of chemical kinetics, turbulent flow, and the uncertainties associated with the igniter energy deposition process. In this work, a detailed model for the growth and stabilization of the hot kernel produced by the igniter is used. Large eddy simulation (LES) is used to describe the turbulent flow and the fuel-air concentration fluctuations, as well as their temporal evolution. Ignition is described as a probabilistic event, with the randomness a result of the uncertainties in turbulent state of the system and the igniter energy deposition. Using an uncertainty quantification approach, the ignition probability is estimated for three different fuels. It is shown that the model correctly reproduces the ignition trends observed in the experiments. Moreover, it is demonstrated that uncertain parameters may be calibrated using related experiments and extended to other operating conditions.
UR - https://www.scopus.com/pages/publications/85083942492
U2 - 10.2514/6.2019-2242
DO - 10.2514/6.2019-2242
M3 - 会议稿件
AN - SCOPUS:85083942492
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -