The shock wave/boundary-layer interaction is a common phenomenon, and it occurs in the
internal and external flow fields of the hypersonic vehicle. Then, the separation, the …

In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …

The shock wave/turbulent boundary layer interaction (SWBLI) exists widely in the internal
and external supersonic flow field. The interaction of shock waves with turbulent boundary …

Boundary layer separation is a common phenomenon in supersonic/hypersonic vehicles,
and can adversely affect the lift coefficient. Currently, active flow control based on microjets …

Shock wave/turbulent boundary layer interactions are widely observed in supersonic flows
with many adverse effects on the flow field, resulting in increasing investigation on their …

Shock-wave/boundary-layer interactions in laminar and fully turbulent boundary layers have
been widely investigated in previous efforts, but relatively little research has been conducted …

In the present article, we establish the numerical solution for the mixed Volterra-Fredholm
integral equation (MV-FIE) in (1+ 1) dimensional in the Banach space L2 [− 1, 1]× C [0, T], T< …

The primary focus of the present survey is to categorize the results of various investigations
on the Shock/Boundary-Layer Interactions (SBLIs), their repercussions, and the effective …

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 …

Supersonic and hypersonic vehicles have complex shock wave/boundary layer interaction
problems during flight, and it adversely affect the aerodynamic performance of the vehicle. In …