The Characteristics of a Cylindrical Probe at High Subsonic Speeds:Part 2: The Case having Inclination Angles
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概要
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In measuring high subsonic internal flows which are observed in high speed turbomachines such as transonic or supersonic compressors, authors planned to use a cylindrical probe which was supported at both ends, and got satisfactory results in the case of zero inclination angle.<BR>Furthermore, the inclination characteristics of this probe were investigated experimentally and it was revealed that the yaw angle of flow could be easily obtained independently of both Mach number M<SUB>∞</SUB> and inclination angle α. It was also revealed that the flow component normal to the axis of the probe (total pressure P<SUB>0</SUB>, Mach number M<SUB>∞</SUB>) could be obtained with a fair accuracy from the characteristics of zero inclination angle within the range of not too large inclination angles (about ±15 degrees).
- 社団法人 日本航空宇宙学会の論文
社団法人 日本航空宇宙学会 | 論文
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