Transonic flow calculations for rigid and flexible wings using a higher- order approximation method
type: Item
instance of: scholarly article
title: Transonic flow calculations for rigid and flexible wings using a higher- order approximation method
zbMATH Open document ID: 0593.76068
DOI: 10.1016/0045-7825(87)90106-X
author: Keyang Shen
author: Xihua Zhang
published in: Computer Methods in Applied Mechanics and Engineering
publication date: 1987-01-01T00:00:00Z
review text: This paper presents the transonic higher-order approximation method. This method is applicable to the transonic flow (in subsonic and low- supersonic free streams) over high and low aspect ratio rigid, flexible thin, and thick wings with or without control deflections. Typical computed results and their comparisons with wind tunnel test data are presented.
Mathematics Subject Classification ID: 76H05
Mathematics Subject Classification ID: 76M99
zbMATH DE Number: 3954531
zbMATH Keywords: difference schemes
zbMATH Keywords: elastic deformation
zbMATH Keywords: wing shape
zbMATH Keywords: flexible thin wing
zbMATH Keywords: thick wings
zbMATH Keywords: hybrid potential equations
zbMATH Keywords: blunt leading edge
zbMATH Keywords: transonic small-disturbance equation
zbMATH Keywords: transonic higher-order approximation method
zbMATH Keywords: low-supersonic free streams
zbMATH Keywords: high and low aspect ratio
zbMATH Keywords: control deflections
MaRDI profile type: Publication
cites work: A second-order approximate method for transonic small-disturbance potential flow and its application to the analysis of flows over airfoils
cites work: Finite difference computation for transonic steady potential flows
full work available at URL: 0045-7825(87)90106-x
OpenAlex ID: W2197834257
description: scientific article; zbMATH DE number 3954531