日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
膨張流中の衝撃波の構造
高尾 吉郎
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ジャーナル フリー

1969 年 17 巻 189 号 p. 382-384

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The structure of the Mach disk in supersonic free jets has been studied by using a static pressure probe. In the low density jets of post nozzle pressure less than 10 torr, the thickness of shock waves is affected by some upstream conditions, but the position of the termination is a function of the nozzle geometry and the pressure ratio as in an inviscid-continuum jet.

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© The Japan Society for Aeronautical and Space Sciences
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