航空宇宙技術
Online ISSN : 1884-0477
ISSN-L : 1884-0477
直流放電場との干渉による衝撃波速度変調効果
松田 淳青山 直樹山崎 将成鈴木 啓太
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ジャーナル フリー

2017 年 16 巻 p. 91-99

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The relationship between the shock wave propagation velocity and the discharge power was investigated by applying the laser schrielen technique for the shock tube experiment at the shock Mach number of 2.17±0.03. The time interval of the shock wave arrival between the two laser beams was 160.5 μsec in the case without the discharged plasma. On the other hand, in the case with the discharged plasma, it was 157.8 μsec at 10.2 W and 149.2 μsec at 73.0 W, respectively. These results suggest that the shock wave propagation velocity can be accelerated with increasing the input power. This tendency agrees with the numerical simulation results, at least qualitatively.

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© 2017 The Japan Society for Aeronautical and Space Sciences
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