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...
Saved in:
主要作者: | |
---|---|
格式: | Thesis |
语言: | English English English |
出版: |
2019
|
主题: | |
在线阅读: | http://eprints.uthm.edu.my/30/1/24p%20MOHD%20FAUZI%20BIN%20YAAKUB.pdf http://eprints.uthm.edu.my/30/2/MOHD%20FAUZI%20BIN%20YAAKUB%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/30/3/MOHD%20FAUZI%20BIN%20YAAKUB%20WATERMARK.pdf |
标签: |
添加标签
没有标签, 成为第一个标记此记录!
|