Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena

DOI10.1016/0045-7930(96)00019-9zbMath0894.76030OpenAlexW2080247290MaRDI QIDQ1370692

J. Ning

Publication date: 9 December 1997

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(96)00019-9

zbMATH Keywords

scaling lawsaerodynamic coefficientsupstream influencecontrol surface deflection angleleading edge shapepeak heatingwing-fuselage junction configurations

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Related Items (6)

Numerical assessment of correlations for shock wave boundary layer interaction ⋮ Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed ⋮ A diffusion-regulated scheme for the compressible Navier-Stokes equations using a boundary-layer sensor ⋮ Time-implicit gas-kinetic scheme ⋮ A pressure-based Mach-uniform method for viscous fluid flows ⋮ Numerical simulation of Görtler vortices in hypersonic compression ramps

Cites Work

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• Damped, direction-dependent multigrid for hypersonic flow computations
• High resolution schemes for hyperbolic conservation laws
• Implicit total variation diminishing (TVD) schemes for steady-state calculations
• Solutions of hypersonic viscous flows with total variation diminishing multigrid techniques
• Multi-Level Adaptive Solutions to Boundary-Value Problems
• Multigrid Techniques for Hypersonic Viscous Flows
• A contribution to the great Riemann solver debate
• Validation procedure for the analysis of shock-wave/boundary-layer interaction problems

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