摘要
An experimental study on the production and development of streamwise vortices in a compressor cascade is reported. At four locations inside and one location outside the blade passage, the mean velocity components, three turbulent intensities and three Reynolds stresses were measured with an 'x' hot wire probe. The results obtained describe the flow structure in the corner between the end-wall and blade suction surface in detail. The mechanism causing the shed corner vortex pair and secondary vortex pair and the effect of these vortices on the cascade losses are discussed.
| 源语言 | 英语 |
|---|---|
| 期刊 | American Society of Mechanical Engineers (Paper) |
| 出版状态 | 已出版 - 1988 |
| 活动 | Unknown conference - Amsterdam, Neth 期限: 6 6月 1988 → 9 6月 1988 |
学术指纹
探究 'EXPERIMENTAL STUDY OF STREAMWISE VORTICES IN A COMPRESSOR CASCADE.' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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