Drag reduction in aircraft model using Elliptical winglet

Drag reduction in aircraft model using Elliptical winglet

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Bibliographic Details
Main Authors: Prithvi, Raj Arora, Assoc. Prof. Dr., A., Hossain, Prasetyo, Edi, Ir., A. A., Jaafar, Thamir S., Younis, M., Saleem
Format: Article
Language:English
Published: The Institution of Engineers, Malaysia 2011
Subjects:
Induced drag
Lift curve slope
Wind tunnel balance
Winglet
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/13549
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Institution: Universiti Malaysia Perlis
Language: English
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