Design optimization of unsteady airfoils with continuous adjoint method
type: Item
instance of: scholarly article
title: Design optimization of unsteady airfoils with continuous adjoint method
zbMATH Open document ID: 1326.76013
author: Liang Fang
author: Xiaowei Li
published in: AMM. Applied Mathematics and Mechanics. (English Edition)
publication date: 2015-11-27T00:00:00Z
Mathematics Subject Classification ID: 76B10
Mathematics Subject Classification ID: 76B75
Mathematics Subject Classification ID: 76M12
zbMATH DE Number: 6514173
zbMATH Keywords: airfoil optimization
zbMATH Keywords: continuous adjoint method
zbMATH Keywords: unsteady flow
MaRDI profile type: Publication
full work available at URL: s10483-015-2010-9
OpenAlex ID: W1193574193
cites work: Aerodynamic design via control theory
cites work: Optimum aerodynamic design using the Navier-Stokes equations
cites work: Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers
cites work: Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
cites work: Optimal aerodynamic design of airfoils in unsteady viscous flows
DOI: 10.1007/S10483-015-2010-9
description: scientific article; zbMATH DE number 6514173