화학공학소재연구정보센터
검색결과 : 6건
No. Article
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