A computational simulation of rotor-fuselage flow interaction in hovering and forward flight

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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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Bibliographic Details
Main Author:	Ismail, Mohamad Hafiz
Format:	Thesis
Language:	English
Published:	2007
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://eprints.utm.my/10052/ http://eprints.utm.my/10052/1/MohamadHafizIsmailMFKM2008.pdf

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