On shock layer method for the hypersonic flow problems
type: Item
instance of: scholarly article
title: On shock layer method for the hypersonic flow problems
zbMATH Open document ID: 0637.76057
DOI: 10.1007/BF02019633
published in: Applied Mathematics and Mechanics. (English Edition)
publication date: 1987-01-01T00:00:00Z
review text: The problem of hypersonic flow around a sharp-nosed slender body is studied for plane or axisymmetric conditions with the assumption that there exists a shock layer in which the density of the gas is very big. A slightly changed Shvez's method [\textit{M. E. Shvez}, Prikl. Mat. Mekh. 13, 257-266 (1949; Zbl 0041.542)] is used to find a zero-order and first- order approximation. Whereas Chernyi's method [\textit{G. G. Chernyi}, Gas flow at high supersonic velocity (1959; Zbl 0090.413) on pp. 125-139] is not applicable for the case \(\gamma =1\), the proposed method remedies this weakness.
reviewed by: Walter Wuest
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76L05
Mathematics Subject Classification ID: 35L67
zbMATH DE Number: 4039490
zbMATH Keywords: hypersonic flow
zbMATH Keywords: sharp-nosed slender body
zbMATH Keywords: shock layer
zbMATH Keywords: first-order approximation
author: Yi-Wu Yuan
MaRDI profile type: Publication
description: scientific article; zbMATH DE number 4039490