The Application of Combined Momentum – Blade Element Theory for Aerodynamics Analysis Helicopter Rotor Blade in the Forward Flight

• المؤلفون الرئيسيون: Ghazirah, Ghazirah, Basuno, B., Razali, Radzuan
• التنسيق: Conference or Workshop Item
• اللغة: English
• منشور في: 2006
• الموضوعات: TL Motor vehicles. Aeronautics. Astronautics
• الوصول للمادة أونلاين: http://eprints.utm.my/id/eprint/356/1/Ghazirah2006_TheApplicationofCombinedMomentum_.pdf; http://eprints.utm.my/id/eprint/356/

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...