Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack
type: Item
instance of: scholarly article
title: Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack
zbMATH Open document ID: 1378.76041
published in: Applied Mathematics and Mechanics. (English Edition)
publication date: 2010-11-23T00:00:00Z
Mathematics Subject Classification ID: 76K05
Mathematics Subject Classification ID: 76N20
zbMATH DE Number: 5818423
author: Jianxin Liu
author: Jisheng Luo
MaRDI profile type: Publication
full work available at URL: s10483-010-0501-z
OpenAlex ID: W2069288366
cites work: Remarks on disputed numerical results in compressible boundary-layer stability theory
cites work: Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers
cites work: Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets
DOI: 10.1007/S10483-010-0501-Z
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description: scientific article; zbMATH DE number 5818423