Application of Reduced Order Models in Aircraft Gust Response Studies

Stephen P I Williams, Dorian P. Jones, Ann L. Gaitonde, Christopher J A Wales, Samantha J. Huntley

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

234 Downloads (Pure)

Abstract

The aim of this paper is to investigate the role Reduce Order Models (ROMs) can play in the early phases of aircraft design. During such periods of design, resources (both in terms of hardware and time) available for Computational Fluid Dynamics (CFD) are at a premium. As gust response cases, which are often critical load cases, are traditionally computationally expensive, a tool that allows for rapid, accurate modelling of such cases would be of great use. This paper first looks at the initial development of such a ROM, before exploring methods by which their computational cost can be further reduced. Ultimately this led to the development of a ROM that, for an inviscid wing model, requires approximately a tenth of the resources required by full order CFD simulation to carry out one gust case, and near negligible cost to model further cases at the same Mach number.

Original languageEnglish
Title of host publication46th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages23
ISBN (Print)9781624104367
DOIs
Publication statusPublished - 13 Jun 2016
Event46th AIAA Fluid Dynamics Conference, 2016 - Washington, United States
Duration: 13 Jun 201617 Jun 2016

Conference

Conference46th AIAA Fluid Dynamics Conference, 2016
CountryUnited States
CityWashington
Period13/06/1617/06/16

Fingerprint Dive into the research topics of 'Application of Reduced Order Models in Aircraft Gust Response Studies'. Together they form a unique fingerprint.

Cite this