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ANSYS FLUENT 2D Transient simulation NACA-23012-33

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Aerodynamics 2D transient simulation in ANSYS FLUENT and comparison results with NACA experiment (Report NACA №610) Нестационарный аэродинамический расчет обтекания профиля NACA-23012-33 в ANSYS FLUENT и сравнения полученых характеристик с отчетом NACA 1935 года.

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