The computational modelling of experiments, with the end aim of providing sufficiently accurate simulations to assess and improve turbulence models is described. Solid wall tunnels are the only tunnels in which the boundary conditions can, in principle, be known exactly. The modelling of the tunnel walls for transonic flows requires the accurate modelling of the viscous displacement effects on the tunnel walls. This paper describes the modelling of semispan wing experiments in solid wall tunnels, with the tunnel walls modelled as inviscid walls, and with all 4 walls modelled viscously. The effect of the viscous effects is discussed, as well as the feasibility of modelling these effects in an inviscid, apriori manner.


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    Titel :

    Computational Simulation of Semispan Wings in Wind Tunnels


    Beteiligte:
    Olsen, Mike (Autor:in) / Rizk, Yehia (Autor:in)

    Kongress:

    AIAA 36th Aerospace Sciences Meeting ; 1998 ; Reno, NV, United States


    Erscheinungsdatum :

    1998-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Computational simulation of a semispan wing in a wind tunnel

    Olsen, Michael / Rizk, Yehia | AIAA | 1998


    Computational Simulation of a Semispan Wing in a Wind Tunnel

    Olsen, M. E. / Rizk, Y. / AIAA | British Library Conference Proceedings | 1998


    Computational Transonic Optimization and Wind-Tunnel Test of a Semispan Wing

    H.P. Haney / E.G. Waggoner / W.F. Ballhaus | AIAA | 1978