Thesis-2009-DeSilva.pdf (12.37 MB)
The flow field induced by a flat plate aerofoil with simulated battle damage
thesis
posted on 2018-08-06, 08:48 authored by R. Suraj I. De SilvaThis investigation looks into the induced surface pressure field and flow field of a 2-D
flat plate aerofoil with simulated battle damage. Enhancing survivability is a major
design criteria for military aircraft designers, and the aerodynamic effects of battle
damage has recently come to the fore as an area that warrants further attention. The
current investigation is in effect a continuation of the battle damage research initiated at
Loughborough University by Irwin, with the ultimate aim of enabling quick and accurate
CFD studies to assess the aerodynamic impact of battle damage on a lifting surface. [Continues.]
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Publisher
© Suraj de SilvaPublisher statement
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/Publication date
2009Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.Language
- en