| 摘要: |
| 根据进气道旋流产生的机理，从进气道设计方面，较为全面地研究了现存飞机进气道旋流的一些防止和抑制措施，将有益于解决工程上由于旋流而造成的进气道与发动机的流场匹配方面的问题。 |
| 关键词: 歼击机 航空发动机 进气道－发动机匹配 进气道气流 流动分布 流场畸变 |
| DOI： |
| 分类号:V231.3 |
| 基金项目: |
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| RESEARCH ON ENGINEERING APPLICATION OF ANTI-SWIRL MEASURES IN ENGINE/INLET COMPATIBILITY |
|
Yang Guocai
|
|
The 611st Research Institute, China Aerospace Corporation, Chengdu, 610092
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| Abstract: |
| Based on the mechanicsm of inlet swirl, the measures to prevent andrestrain the inlet swirl of present aircraft in an all-round way from the inlet designpoint of view are studied’ It is hoped that the author’s thinking will benefit the solution of the problems in engine/inlet compatibility arising from swirl’ |
| Key words: Fighter aircraft Aircraft engine Inlet-engine matching Inlet flow Flow distribution Flow distortion |
