Highly cited literature of high-speed compressible flow research

Experimental study of mixing enhancement using pylon in supersonic flow

“…In an Experimental study , Arun Kumar and Rathakrishnan, [38] they observed that mixing capability of truncated triangular tabs with semicircular corrugated tabs assumes a maximum having adverse pressure gradient of around 10% and performance of all tabs were effective only in near field of the jets at all expansions levels. A collection of compressible flow research has been presented by Kostoff and Cummings [39]. In an experimental and computational study by Doster et al [40] three different geometries were compared and found that ramp pylon and alternating wedge Pylon introduce stream-wise vorticity into the flow to increase mixing action.…”

Wall modeled large eddy simulation of supersonic flow physics over compression–expansion ramp

“…Shock-turbulent boundary layer interaction (STBLI) is one of the most prevalent physical phenomena in a variety of applications in aerospace science including supersonic and hypersonic transport, which can affect significantly the aero-thermodynamic loads [2]. Accordingly, the design process of supersonic and hypersonic air vehicles requires accurate investigation.…”

Study of linear ablative rate of D6AC steel wing used on supersonic missile

“…When the supersonic jet interacts with the aircraft, the compression and friction will produce high temperature in the boundary-layer around the aircraft that damage the surface material. In recent years, the aerodynamic heating of supersonic missiles has attracted wide attention, researchers at home and abroad have carried out a lot of work [1][2][3][4][5][6]. Liu et al [7] analyzed the aerodynamic heating of the supersonic missile wing under the condition of low and medium supersonic (Ma < 5) flight.…”