Aerodynamic analysis of groove based vortex trap configuration on the retreating helicopter blade

The issue of high angle of attacks at the retreating blade receives attention from countless researchers because it is an important factor in the stability of the helicopter. The retreating blade stall will effect the stability of the helicopter due to the high angle of attacks. Prouty‟s helicopter...

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主要作者: Yaakub, Mohd Fauzi
格式: Thesis
语言:English
English
English
出版: 2019
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