Helicopter Blade Stability Analysis Using Aeroelastic Frequency Response Functions
In the present paper, the aeroelastic stability of helicopter rotor blade is determined using Aeroelastic Frequency Response Function. The aeroelastic model of blade is obtained by combining Dowell - Hodges beam model with Loewy unsteady aerodynamic theory which considers an unsteady wake beneath th...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Shahid Chamran University of Ahvaz
2015-07-01
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| Series: | Journal of Applied and Computational Mechanics |
| Online Access: | http://jacm.scu.ac.ir/article_11076.html |