A computational simulation of rotor-fuselage flow interaction in hovering and forward flight
A helicopter rotor-fuselage flow interaction has been studied theoretically and numerically. The study began with the analysis of the induced velocity by helicopter rotor both in hovering and forward flight by using Momentum Theory, Blade Element Theory and Blade Element Momentum Theory. Three-dimen...
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| Format: | Thesis |
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2007-07.
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| Online Access: | Get fulltext |