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

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...

Full description

Bibliographic Details
Main Authors: Ghazirah, Ghazirah, Basuno, B., Razali, Radzuan
Format: Conference or Workshop Item
Language:English
Published: 2006
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
Online Access:http://eprints.utm.my/356/
http://eprints.utm.my/356/1/Ghazirah2006_TheApplicationofCombinedMomentum_.pdf

Similar Items

Similar Items