高超声速运载器宽速域气动/推进耦合建模与分析
程锋1,2(
),张栋1,2,*(),唐硕1,2
),张栋1,2,*(),唐硕1,2
Aerodynamics/propulsion coupled modeling and analysis of hypersonic vehicle within wide speed range
Feng CHENG1,2(),Dong ZHANG1,2,*(),Shuo TANG1,2
),Dong ZHANG1,2,*(),Shuo TANG1,2
图 10. 飞行马赫数、攻角、燃料当量比对运载器推力的影响
Fig.10. Effects of Mach number, angle of attack and fuel equivalence ratio on propulsion of vehicle
