A fast iterative inverse method for turbomachinery blade design
type: Item
instance of: scholarly article
title: A fast iterative inverse method for turbomachinery blade design
zbMATH Open document ID: 1258.76130
author: Yanyan Li
published in: Mechanics Research Communications
publication date: 2013-03-05T00:00:00Z
Mathematics Subject Classification ID: 76N25
Mathematics Subject Classification ID: 76M25
zbMATH DE Number: 6141388
zbMATH Keywords: inverse method
zbMATH Keywords: blade design
zbMATH Keywords: Euler equations
zbMATH Keywords: compressible flow
zbMATH Keywords: turbomachinery
MaRDI profile type: Publication
full work available at URL: j.mechrescom.2009.01.008
OpenAlex ID: W2013508241
cites work: Iterative use of a time-marching code for designing turbomachine blade rows
cites work: Solvability condition and its application to fast numerical solution of overposed inverse problems in compressible flows
cites work: Q5844313
cites work: Q3409553
cites work: Role of constraints in inverse design for transonic airfoils
DOI: 10.1016/J.MECHRESCOM.2009.01.008
description: scientific article; zbMATH DE number 6141388