Please use this identifier to cite or link to this item:
Type: Thesis
Title: Optimal lifting surfaces, including end plates, ground effect & thickness / David William Fin Standingford.
Author: Standingford, David William Fin
Issue Date: 1997
School/Discipline: Dept. of Applied Mathematics
Abstract: The task of calculating the aerodynamic load distribution on a thin three-dimensional lifting surface or wing of finite aspect ratio at small angle of attack presents difficulties for most numerical methods. The two-dimensional lifting-surface integral equation that must be solved is highly singular, and does not possess analytic solutions, even for simple plan-form geometries such as rectangles or ellipses.
Dissertation Note: Thesis (Ph.D.)--University of Adelaide, Dept. of Applied Mathematics, 1998
Subject: Numerical analysis.
Aerodynamic load.
Description: Bibliography: leaves 164-172.
xii, 172 leaves : ill. (some col.) ; 30 cm.
Provenance: This electronic version is made publicly available by the University of Adelaide in accordance with its open access policy for student theses. Copyright in this thesis remains with the author. This thesis may incorporate third party material which has been used by the author pursuant to Fair Dealing exception. If you are the author of this thesis and do not wish it to be made publicly available, or if you are the owner of any included third party copyright material you wish to be removed from this electronic version, please complete the take down form located at:
Appears in Collections:Research Theses

Files in This Item:
File Description SizeFormat 
01front.pdf80.77 kBAdobe PDFView/Open
02whole.pdf9.73 MBAdobe PDFView/Open

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.