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Computational Study of the Aeroelastic Equilibrium Configuration of a Swept Wind Tunnel Wing Model in Subsonic Flow

In: High Performance Computing in Science and Engineering ’06

Author

Listed:
  • L. Reimer

    (RWTH Aachen, Lehrstuhl für Computergestützte Analyse Technischer Systeme (CATS))

  • C. Braun

    (RWTH Aachen, Lehr- und Forschungsgebiet für Mechanik (LFM))

  • J. Ballmann

    (RWTH Aachen, Lehr- und Forschungsgebiet für Mechanik (LFM))

Abstract

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.

Suggested Citation

  • L. Reimer & C. Braun & J. Ballmann, 2007. "Computational Study of the Aeroelastic Equilibrium Configuration of a Swept Wind Tunnel Wing Model in Subsonic Flow," Springer Books, in: Wolfgang E. Nagel & Willi Jäger & Michael Resch (ed.), High Performance Computing in Science and Engineering ’06, pages 421-434, Springer.
    • Handle: RePEc:spr:sprchp:978-3-540-36183-1_31
    DOI: 10.1007/978-3-540-36183-1_31
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