검색결과 : 6건
No. | Article |
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1 |
Performance evaluation of a turbojet engine integrated with interstage turbine burner and solid oxide fuel cell Ji ZX, Qin J, Cheng KL, Liu H, Zhang SL, Dong P Energy, 168, 702, 2019 |
2 |
Efficiency, thrust, and fuel consumption optimization of a subsonic/sonic turbojet engine Patel V, Savsani V, Mudgal A Energy, 144, 992, 2018 |
3 |
Thermodynamic spectrum of direct precooled airbreathing propulsion Yu XF, Pan X, Zheng JL, Wang C, Yu DR Energy, 135, 777, 2017 |
4 |
Thermodynamic analysis on optimum performance of scramjet engine at high Mach numbers Zhang D, Yang SB, Zhang SL, Qin J, Bao W Energy, 90, 1046, 2015 |
5 |
Thermodynamic analysis on specific thrust of the hydrocarbon fueled scramjet Yang QC, Chang JT, Bao W Energy, 76, 552, 2014 |
6 |
Study on combustion mode transition of hydrogen fueled dual-mode scramjet engine based on thermodynamic cycle analysis Cao RF, Chang JT, Tang JF, Wang ZQ, Yu DR International Journal of Hydrogen Energy, 39(36), 21251, 2014 |