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 9. 飞行马赫数和攻角对进气道总压恢复系数和质量流量捕获量的影响
Fig.9. Effects of Mach number and angle of attack on total pressure recovery coefficient and mass flow capture of inlet
