CFD ANALYSIS OF THE EFFECT OF PARABOLIC TAPER DISTRIBUTION OF AN UNTWISTED HELICOPTER ROTOR BLADE
The effect of parabolic taper distribution along the span of a helicopter rotor blade is analyzed in terms of the rotor thrust, torque and Figure of Merit. Various maximum chord length values are investigated. The Reynolds Averaged Navier-Stokes computations are done using the FINE/Turbo flow solver...
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| Главные авторы: | , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
Turkish Air Force Academy
2018-07-01
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| Серии: | Havacılık ve Uzay Teknolojileri Dergisi |
| Предметы: | |
| Online-ссылка: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/289/275 |
| Метки: |
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