Features of start-up processes of a vacuum supersonic tube
N P Savishenko, Артем Васильевич Шевченко, S A Poniaev, K V Tverdohlebov, Евгений Алексеевич Прокопенко, Sergey Yashkov
Abstract
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N P Savishenko, Артем Васильевич Шевченко, S A Poniaev, K V Tverdohlebov, Евгений Алексеевич Прокопенко, Sergey Yashkov
Abstract
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At present experimental gas-dynamic studies of supersonic flows mainly use complex experimental facilities, such as aerodynamic wind tunnels and shock tubes. However, in order to study supersonic flows with Mach numbers M < 4, a vacuum wind tunnel (which is much simpler) can also be used. This paper is concerned with starting processes occurring in a vacuum wind tunnel.
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At present experimental gas-dynamic studies of supersonic flows mainly use complex experimental facilities, such as aerodynamic wind tunnels and shock tubes. However, in order to study supersonic flows with Mach numbers M < 4, a vacuum wind tunnel (which is much simpler) can also be used. This paper is concerned with starting processes occurring in a vacuum wind tunnel.
Key concepts: Supersonic speed, Supersonic wind tunnel, Aerodynamics, Mach number, Wind tunnel, Mechanics, Choked flow, Aerospace engineering