Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies
type: Item
instance of: scholarly article
title: Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies
zbMATH Open document ID: 1373.76075
DOI: 10.1134/S0015462817040111
author: I. G. Brykina
published in: Fluid Dynamics
publication date: 2017-11-06T00:00:00Z
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76L05
Mathematics Subject Classification ID: 76V05
Mathematics Subject Classification ID: 80A20
zbMATH DE Number: 6803047
zbMATH Keywords: three-dimensional hypersonic flow
zbMATH Keywords: heat flux
zbMATH Keywords: blunt body
zbMATH Keywords: analytical solution
zbMATH Keywords: ideal catalytic surface
MaRDI profile type: Publication
cites work: Q5334985
cites work: Investigation of three-dimensional boundary layers on blunt bodies with permeable surface
cites work: Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow
cites work: Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry
cites work: Integration of hypersonic viscous shock layer equations by a successive approximation method
cites work: Comparison of approximate analytical and numerical solutions for heat fluxes in viscous supersonic flow past a body
cites work: Q5731719
cites work: Q3259465
cites work: Q5621197
full work available at URL: s0015462817040111
OpenAlex ID: W2745486319
description: scientific article; zbMATH DE number 6803047