The Aerodynamic Analysis of Rotary Wing Blade Flapping and Wake Dynamics Coupled System
碩士 === 淡江大學 === 機械工程學系 === 84 === An analytic model and numerical scheme have been developed to predict the aerodynamic loads on helicopter rotors due to various blade chord length in hover and forward flight. The Peters'' finite state inflow th...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1996
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| Online Access: | http://ndltd.ncl.edu.tw/handle/39615615589932730186 |