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    Prediction of vortex lift on interacting delta wings in incompressible flow (1984)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Vortex flow modeling is used to calculate the steady inviscid incompressible flow past one, two and three delta wing configurations. The wings are modeled with vortex lattices and the leading and trailing-edge sheets are modeled by segmented straight vortex filaments. Aerodynamic characteristics are obtained for a range of geometry and angle of attack.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 84-0136
    Format: text
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