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 12. 飞行马赫数、攻角、副翼舵偏角和燃料当量比对运载器俯仰力矩系数的影响
Fig.12. Effects of Mach number, angle of attack, deflection angle of aileron and fuel equivalence ratio on pitch moment coefficient of vehicle
