An inverse method for subcritical flows
type: Item
instance of: scholarly article
title: An inverse method for subcritical flows
zbMATH Open document ID: 0587.76092
DOI: 10.1016/0021-9991(86)90196-8
author: Prabir Daripa
author: Lawrence Sirovich
published in: Journal of Computational Physics
publication date: 1986-01-01T00:00:00Z
review text: The inverse problem in the tangent gas approximation is considered. An exact method for designing airfoils is presented. Constraints on the speed distribution are easily implemented. A simple numerical algorithm which is fast and accurate is presented. Comparison of designed airfoils using the tangent gas method with exact Euler results is found to be excellent for subcritical flows.
Mathematics Subject Classification ID: 76G25
Mathematics Subject Classification ID: 76M99
Mathematics Subject Classification ID: 76N15
zbMATH DE Number: 3943368
zbMATH Keywords: two-dimensional subsonic flow
zbMATH Keywords: inverse problem
zbMATH Keywords: tangent gas approximation
zbMATH Keywords: exact method for designing airfoils
zbMATH Keywords: Constraints on the speed distribution
zbMATH Keywords: exact Euler results
zbMATH Keywords: subcritical flows
MaRDI profile type: Publication
full work available at URL: 0021-9991(86)90196-8
OpenAlex ID: W2142070831
cites work: Q5844313
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cites work: Two-Dimensional Subsonic Flow of Compressible Fluids
cites work: Q3016244
cites work: Q3245943
description: scientific article; zbMATH DE number 3943368