The flow field about a delta wing equipped with thrust reverse jets in slow speed flight near the ground has been computed. Results include the prediction of the flow about the delta wing at four fixed heights above the ground, and simulated landing, in which the delta wing descends towards the ground. Comparison of computed and experimental lift coefficients indicates that the simulations can capture at least the qualitative trends in lift-loss encountered by thrust-vectoring aircraft operating in ground effect.


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    Title :

    Numerical simulation of a powered-lift landing


    Contributors:


    Publication date :

    1993-11-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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