Influence of intense surface cooling on hypersonic viscous flow past a delta wing
type: Item
instance of: scholarly article
title: Influence of intense surface cooling on hypersonic viscous flow past a delta wing
zbMATH Open document ID: 0934.76035
DOI: 10.1007/BF02698215
author: G. N. Dudin
published in: Fluid Dynamics
publication date: 2000-04-13T00:00:00Z
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 80A20
zbMATH DE Number: 1339991
zbMATH Keywords: perfect gas
zbMATH Keywords: semi-infinite thin delta wing
zbMATH Keywords: laminar boundary layer
zbMATH Keywords: strong viscous-inviscid interaction
zbMATH Keywords: power-law shape
MaRDI profile type: Publication
cites work: Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow
cites work: On the existence of self-similar solutions in the supercritical region on a delta wing in a hypersonic flow
cites work: Q5526804
cites work: On the outer-edge problem of a hypersonic boundary layer
cites work: A method of calculating a regime of strong viscous interaction on a delta wing
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description: scientific article; zbMATH DE number 1339991