Singularities of the flow field in the neighborhood of the windward surface of a small aspect ratio delta wing in hypersonic stream
type: Item
instance of: scholarly article
title: Singularities of the flow field in the neighborhood of the windward surface of a small aspect ratio delta wing in hypersonic stream
zbMATH Open document ID: 1478.76047
DOI: 10.1134/S0015462821050037
author: V. N. Golubkin
published in: Fluid Dynamics
publication date: 2021-11-26T00:00:00Z
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76L05
Mathematics Subject Classification ID: 76M45
zbMATH DE Number: 7434442
zbMATH Keywords: attached shock wave
zbMATH Keywords: detached shock wave
zbMATH Keywords: asymptotic thin shock layer method
zbMATH Keywords: singular cross-section
zbMATH Keywords: concentrated force
zbMATH Keywords: entropy layer
MaRDI profile type: Publication
cites work: Q3254130
cites work: Q4068361
cites work: LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
cites work: Three-dimensional hypersonic gas flow over wings
cites work: Q5526804
cites work: Q5629380
cites work: Q3835198
cites work: Thickness effect on the force of slender delta wings in hypersonic flow
cites work: Recent Hypersonic Studies of Wings and Bodies
cites work: Q5509552
full work available at URL: s0015462821050037
OpenAlex ID: W3202509743
description: scientific article; zbMATH DE number 7434442