Impact of shock wave boundary layer interaction on the internal flow and performance of scramjet intake

DOI10.1134/S0015462821060069zbMath1483.76034OpenAlexW3216704475MaRDI QIDQ2668122

Yanyan Li

Publication date: 3 March 2022

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462821060069

zbMATH Keywords

shock wavecompressible Navier-Stokes equationsboundary layerhypersonic flowheat fluxseparation bubblecentral-upwind scheme

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05) Basic methods in fluid mechanics (76M99) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Compressible Navier-Stokes equations (76N06)

Cites Work

• Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions
• Shock Wave-Boundary-Layer Interactions

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