Computational study of the aeroelastic equilibrium configuration of a swept wind tunnel wing model in subsonic flow
- In the Collaborative Research Center SFB 401 at RWTH Aachen University, the numerical aeroelastic method SOFIA for direct numerical aeroelastic simulation is being progressively developed. Numerical results obtained by applying SOFIA were compared with measured data of static and dynamic aeroelastic wind tunnel tests for an elastic swept wing in subsonic flow.
| Author: | Lars Reimer, Carsten BraunORCiD, Josef Ballmann |
|---|---|
| ISBN: | 978-3-540-36165-7 |
| Parent Title (English): | High performance computing in science and engineering '06. Transactions of the High Performance Computing Center Stuttgart (HLRS) 2006 / Wolfgang E. Nagel ... Eds. |
| Publisher: | Springer |
| Place of publication: | Berlin [u.a.] |
| Document Type: | Part of a Book |
| Language: | English |
| Year of Completion: | 2007 |
| Date of the Publication (Server): | 2013/06/21 |
| First Page: | 421 |
| Last Page: | 434 |
| Link: | http://link.springer.com/chapter/10.1007/978-3-540-36183-1_31 |
| Zugriffsart: | bezahl |
| Institutes: | FH Aachen / Fachbereich Luft- und Raumfahrttechnik |
| collections: | Verlag / Springer |
