Estimating vertical drag on helicopter fuselage during hovering

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Estimating vertical drag on helicopter fuselage during hovering

This research aims at prediction of aerodynamic drag on a conventional helicopter fuselage, EC-120. The drag has been evaluated using theoretical method which is aircraft elements method [1] and numerical method which is using commercial software Fluent 6.2 [2]. The two results are found to be in go...

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Bibliographic Details
Main Authors:	Wahab, A. A., Ismail, M. Hafiz
Format:	Conference or Workshop Item
Language:	English
Published:	2006
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.utm.my/296/ http://eprints.utm.my/296/1/AAWahab2006_EstimatingVerticalDragonHelicopter.pdf

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