The Dynamic Analysis of Coupled Rotor System With Dynamic Stall
碩士 === 淡江大學 === 航空太空工程學系 === 89 === For a rotor blade in forward flight, a high angle of attack often is encountered in normal operating conditions. If the angle of attack of the blade sections becomes large enough, dynamic stall may occur. Typically, this occurs on the retreating blade. In a hov...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2001
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| Online Access: | http://ndltd.ncl.edu.tw/handle/82081079710850066182 |