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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    Title :

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


    Contributors:
    vanDam, C. P. (author) / Saephan, S. (author) / Fremaux, C. M. (author) / DalBello, T. (author)


    Publication date :

    2003-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English