Modeling the Flow Around a Delta Wing Partially Made of Permeable Material


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Mathematical modeling of a supersonic gas flow around a delta wing at M=2 has been carried out. A wing made of a conventional solid material was compared with a wing whose leading edge was made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.

delta wing, gas dynamics, computational aerodynamics, porous materials

DOI: http://doi.org/10.33257/PhChGD.24.5.1070


Volume 24, issue 5, 2023 year


Моделирование обтекания треугольного крыла, частично изготовленного из проницаемого материала

Выполнено математическое моделирование обтекания треугольного крыла сверхзвуковым потоком газа при М=2. Сравнивались крыло, изготовленное из обычного сплошного материала, и крыло, передняя кромка которого выполнена из пористого материала с коэффициентом пористости 0.6. Исследовано влияние проницаемой кромки на структуру течения и тепловой режим.

треугольное крыло, газовая динамика, вычислительная аэродинамика, пористые материалы.

DOI: http://doi.org/10.33257/PhChGD.24.5.1070


Volume 24, issue 5, 2023 year



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