Abstract
Recent studies have pointed out that conventional lifting rotors in forward flight have efficiencies far lower than the optimum efficiencies predicted by theory. This paper presents a closed-form optimization of induced power with finite-state models is expanded to obtain the results for pressure and induced velocity distributions for a rotor in forward flight. Results for induced power efficiency (IPE) variations in forward flight and for different conditions are presented.
| Original language | English |
|---|---|
| Journal | Collection of Technical Papers - AIAA Applied Aerodynamics Conference |
| DOIs | |
| State | Published - 2009 |
| Event | 27th AIAA Applied Aerodynamics Conference - San Antonio, TX, United States Duration: Jun 22 2009 → Jun 25 2009 |
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