The paper summarizes recent developments in boundary layer suction for high-speed air
intakes. Bleed has been efficiently used in supersonic and hypersonic intakes for three …

针对吸气式高超声速飞行器进气道不起动引起飞行器气动特性大范围变化,
从而导致响应出现大幅振荡甚至控制系统失稳的问题, 提出了一种考虑进气道不起动影响的模型 …

I. Introduction cramjet and rocket propulsion systems are the major options for an aircraft to
operate in high Mach number regime, scramjets having higher specific impulse than rockets …

A comprehensive study on inlet unstart and its control via boundary-layer suction in a dual-
mode scramjet is conducted. The current work encompasses 1) modeling effort of boundary …

A large-scale change in the aerodynamic characteristics of the aircraft caused by the inlet
unstart of the air-breathing hypersonic vehicle causes a large oscillation of the response or …