流体工学部門講演会講演論文集
Online ISSN : 2424-2896
セッションID: 808
会議情報
0808 膨張波管を用いた印加磁場による再突入機の抗力増大効果の実験的検証
渡部 竜平嶋津 悠介服部 盛正永田 靖典山田 和彦安部 隆士手塚 亜聖
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会議録・要旨集 フリー

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The aerodynamic force enhancement effect occurs by applying magnetic field around a reentry vehicle in a weekly-ionized flow behind the strong detached shock wave. Recently, this force enhancement effect was experimentally investigated using an expansion tube which can produce high speed and high enthalpy flow. Because aerodynamic force measurement is difficult due to short test flow period in expansion tube, drag measurement system which employed a piezofilm with fast responsiveness was developed in this study. This drag measurement system was calibrated using CO2 pulse laser and applied to experimental investigation on the aerodynamic force enhancement effect in expansion tube. The aerodynamic force acting on simple models in the flow produced by the expansion tube can be measured in this system. Additionally, the increase of the drag force due to magnetization in a weekly-ionized flow was observed.
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