The Application of Combined Momentum – Blade Element Theory for Aerodynamics Analysis Helicopter Rotor Blade in the Forward Flight
Present work introduced the aerodynamics analysis of rotor blade helicopter in forward flight. The analysis used a combination between a Momentum Theory and The Blade Element Theory. Here the inflow ratio was assumed a uniform over the disk plane and it was predicted by using the momentum Theory. As...
محفوظ في:
المؤلفون الرئيسيون: | Ghazirah, Ghazirah, Basuno, B., Razali, Radzuan |
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التنسيق: | Conference or Workshop Item |
اللغة: | English |
منشور في: |
2006
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الموضوعات: | |
الوصول للمادة أونلاين: | http://eprints.utm.my/id/eprint/356/1/Ghazirah2006_TheApplicationofCombinedMomentum_.pdf http://eprints.utm.my/id/eprint/356/ |
الوسوم: |
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