The University of Southampton
University of Southampton Institutional Repository

Real-time computational fluid dynamics for flight simulation

Real-time computational fluid dynamics for flight simulation
Real-time computational fluid dynamics for flight simulation
A service oriented architecture is described that enables computational fluid dynamics (CFD) simulations to run alongside a human-in-the-loop flight simulator; thereby informing the behavior of a simulated aircraft whilst it is being piloted. The scenario of a helicopter landing on a moving ship at sea, is used as an example application.
A generic service-oriented architecture is presented that allows coupling of a real-time flight simulator, flight dynamics model and CFD simulation running on a high performance computer. The case study used is performing unsteady CFD calculations used to model the aerodynamic development of, and interaction between, the ship and helicopter wakes; The CFD code resides on a cluster computer and is exposed to a PC-based flight simulator as a service, enabling two-way data exchange between the CFD and flight model whilst the simulation is running. Real-time analysis of the CFD results and control inputs allows prediction of the forces acting on the helicopter rotor, this is fed into a full six degree of freedom flight model. Performance results for the full end-to-end architecture are presented to demonstrate the capability, and limitations, of this approach.
The paper concludes with a short discussion regarding the potential for this architecture to provide a generic representation of aircraft-environment interactions, and their influence on performance and handling. Implementing a more accurate representation of these phenomena in flight simulators could improve the ability to prepare pilots for challenging tasks such as: landing on ships, flying in urban environments, dealing with „brown-out? conditions, and encountering the wakes of other aircraft.
computational fluid dynamics, cfd, real-time, helicopter, flight simulation, high performance computing, hpc, i/itsec, coupled, service oriented architecture, soa
Kenny, James
d7a85f06-8163-4d73-9a3d-d2df38ac9015
Takeda, Kenji
e699e097-4ba9-42bd-8298-a2199e71d061
Thomas, Glyn
bccfa8da-6c8b-4eec-b593-00587d3ce3cc
Kenny, James
d7a85f06-8163-4d73-9a3d-d2df38ac9015
Takeda, Kenji
e699e097-4ba9-42bd-8298-a2199e71d061
Thomas, Glyn
bccfa8da-6c8b-4eec-b593-00587d3ce3cc

Kenny, James, Takeda, Kenji and Thomas, Glyn (2008) Real-time computational fluid dynamics for flight simulation. The Interservice/Industry Training, Simulation & Education Conference (I/ITSEC), Orlando, USA. 01 - 04 Dec 2008. 8 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

A service oriented architecture is described that enables computational fluid dynamics (CFD) simulations to run alongside a human-in-the-loop flight simulator; thereby informing the behavior of a simulated aircraft whilst it is being piloted. The scenario of a helicopter landing on a moving ship at sea, is used as an example application.
A generic service-oriented architecture is presented that allows coupling of a real-time flight simulator, flight dynamics model and CFD simulation running on a high performance computer. The case study used is performing unsteady CFD calculations used to model the aerodynamic development of, and interaction between, the ship and helicopter wakes; The CFD code resides on a cluster computer and is exposed to a PC-based flight simulator as a service, enabling two-way data exchange between the CFD and flight model whilst the simulation is running. Real-time analysis of the CFD results and control inputs allows prediction of the forces acting on the helicopter rotor, this is fed into a full six degree of freedom flight model. Performance results for the full end-to-end architecture are presented to demonstrate the capability, and limitations, of this approach.
The paper concludes with a short discussion regarding the potential for this architecture to provide a generic representation of aircraft-environment interactions, and their influence on performance and handling. Implementing a more accurate representation of these phenomena in flight simulators could improve the ability to prepare pilots for challenging tasks such as: landing on ships, flying in urban environments, dealing with „brown-out? conditions, and encountering the wakes of other aircraft.

This record has no associated files available for download.

More information

Published date: December 2008
Venue - Dates: The Interservice/Industry Training, Simulation & Education Conference (I/ITSEC), Orlando, USA, 2008-12-01 - 2008-12-04
Keywords: computational fluid dynamics, cfd, real-time, helicopter, flight simulation, high performance computing, hpc, i/itsec, coupled, service oriented architecture, soa
Organisations: Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 64868
URI: http://eprints.soton.ac.uk/id/eprint/64868
PURE UUID: 11b32a7f-f104-4223-9974-e2c3c5eb56a0

Catalogue record

Date deposited: 20 Jan 2009
Last modified: 11 Dec 2021 18:26

Export record

Contributors

Author: James Kenny
Author: Kenji Takeda
Author: Glyn Thomas

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×