A Reynolds-average Navier Stokes method developed for rotorcraft type of flow problems is applied for predicting the forces and moments of forebody models at high-angle-of-attack dynamic conditions and for providing insight into the flow characteristics at these conditions. Wind-tunnel results from rotary testing on generic forebody models conducted by NASA Langley and DERA are used for comparison. This paper focuses on the steady-state flow problem.


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    Titel :

    Prediction of Flows about Forebodies at High-Angle-of-Attack Dynamic Conditions


    Beteiligte:
    vanDam, C. P. (Autor:in) / Saephan, S. (Autor:in) / Fremaux, C. M. (Autor:in) / DalBello, T. (Autor:in)


    Erscheinungsdatum :

    01.03.2003


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Prediction of Flows about Forebodies at High-Angle-of-Attack Dynamic Conditions

    C. P. van Dam / S. Saephan / C. M. Fremaux et al. | NTIS | 2004


    Lateral Aerodynamics Characteristics of Forebodies at High Angle of Attack in Subsonic and Transonic Flows

    Koren, S. / Arieli, R. / Rom, J. | British Library Online Contents | 1992




    Simulation of Flow About Rotating Forebodies at High Angles of Attack

    S. Saephan / C. P. van Dam / C. Fremaux et al. | AIAA | 2004