TY - JOUR
T1 - Numerical Simulation Study on Injection and Mixing Characteristics of Supercritical RP-3 Aviation Kerosene
AU - Liu, Penghui
AU - Wang, Zhisheng
AU - Shi, Pengyu
AU - Fan, Wei
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2023
Y1 - 2023
N2 - A real gas calculation model is developed using the P-R equation of state to investigate the injection and mixing characteristics of supercritical RP-3 aviation kerosene in the combustion chamber. In this investigation, n-decane is used as an alternative fuel, and the physical parameters of n-decane at the supercritical state are calculated. The jet and mixing characteristics of supercritical kerosene in different combustion chamber models are investigated by this calculation model. The combustion chamber head configuration suitable for supercritical kerosene is obtained by analyzing the spatial inhomogeneity, the deviation of equivalent ratio fluctuation, and the mixing degree.
AB - A real gas calculation model is developed using the P-R equation of state to investigate the injection and mixing characteristics of supercritical RP-3 aviation kerosene in the combustion chamber. In this investigation, n-decane is used as an alternative fuel, and the physical parameters of n-decane at the supercritical state are calculated. The jet and mixing characteristics of supercritical kerosene in different combustion chamber models are investigated by this calculation model. The combustion chamber head configuration suitable for supercritical kerosene is obtained by analyzing the spatial inhomogeneity, the deviation of equivalent ratio fluctuation, and the mixing degree.
UR - http://www.scopus.com/inward/record.url?scp=85152618582&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/2457/1/012006
DO - 10.1088/1742-6596/2457/1/012006
M3 - 会议文章
AN - SCOPUS:85152618582
SN - 1742-6588
VL - 2457
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012006
T2 - 2022 2nd International Conference on Mechatronics Technology and Aerospace Engineering, ICMTAE 2022
Y2 - 4 November 2022 through 6 November 2022
ER -