Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena
type: Item
instance of: scholarly article
title: Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena
zbMATH Open document ID: 0894.76030
DOI: 10.1016/0045-7930(96)00019-9
author: J. Ning
published in: Computers and Fluids
publication date: 1997-12-09T00:00:00Z
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76L05
Mathematics Subject Classification ID: 76M25
zbMATH DE Number: 1079033
zbMATH Keywords: scaling laws
zbMATH Keywords: wing-fuselage junction configurations
zbMATH Keywords: control surface deflection angle
zbMATH Keywords: leading edge shape
zbMATH Keywords: upstream influence
zbMATH Keywords: peak heating
zbMATH Keywords: aerodynamic coefficients
MaRDI profile type: Publication
full work available at URL: 0045-7930(96)00019-9
OpenAlex ID: W2080247290
cites work: Q5847971
cites work: Validation procedure for the analysis of shock-wave/boundary-layer interaction problems
cites work: Multigrid Techniques for Hypersonic Viscous Flows
cites work: Solutions of hypersonic viscous flows with total variation diminishing multigrid techniques
cites work: High resolution schemes for hyperbolic conservation laws
cites work: Implicit total variation diminishing (TVD) schemes for steady-state calculations
cites work: Multi-Level Adaptive Solutions to Boundary-Value Problems
cites work: Damped, direction-dependent multigrid for hypersonic flow computations
cites work: A contribution to the great Riemann solver debate
description: scientific article; zbMATH DE number 1079033