Discussion of Mach Number Effects shock patterns force behaviour Drag rise

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  • Опубликовано: 11 сен 2024

Комментарии • 1

  • @francescocandian2708
    @francescocandian2708 3 года назад

    Hi, I have a question: After we reach MCrit and get a shockwave, what happens to the position of such shockwave on the top surface of the profile as we increase the Angle of Attack (for instance by changing the camber, i.e. lowering an aileron)? Does it move towards the leading edge or towards the trailing edge of the profile? Could you please explain why? Is there a graph/picture somewhere?