Control of shock-wave/boundary-layer interaction using a backward-facing step
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. Direct numerical simulations of supersonic compression-expansion slope with a multi-GPU parallel algorithm;Xu;Acta Astronaut.,2021
2. Wall temperature effects on shock wave/turbulent boundary layer interaction via direct numerical simulation;Zhu;Acta Astronaut.,2021
3. Experimental study of swept impinging oblique shock/boundary-layer interactions;Padmanabhan;AIAA J.,2020
4. Hypersonic oscillating shock-wave/boundary-layer interaction on a flat plate;Currao;AIAA J.,2021
5. Low-frequency unsteadiness mechanisms in shock wave/turbulent boundary layer interactions over a backward-facing step;Hu;J. Fluid Mech.,2021
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1. Design and aerodynamic characteristics of variable-geometry hypersonic inlet based on shock wave elimination;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-06-23
2. Numerical investigations on interactions between 2D/3D conical shock wave and axisymmetric boundary layer at Ma=2.2;Aerospace Science and Technology;2024-01
3. Surrogate-based optimization on bump for shock wave/boundary layer interaction control;Acta Astronautica;2023-11
4. Assessment of Total Pressure and Swirl Distortions in a Busemann Inlet at Mach 6;Journal of Applied Fluid Mechanics;2023-09-01
5. Study on the separation in the shock wave/boundary layer interaction induced by a curved fin;Physics of Fluids;2023-07-01
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