Performance Analysis Of A Compliant Wing For A Light Aircraft

Main purpose of this project is to apply the compliant mechanism into aircraft wing. It can improve the flight performance of conventional light aircraft. A compliant mechanism is flexible structure that elastically deforms without joints to produce a desired force or displacement. This study...

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Bibliographic Details
Main Author: Mohamad Sidik, Mohamad Sabri
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2005
Subjects:
Online Access:http://eprints.usm.my/58203/1/Performance%20Analysis%20Of%20A%20Compliant%20Wing%20For%20A%20Light%20Aircraft_Mohamad%20Sabri%20Mohamad%20Sidik.pdf
http://eprints.usm.my/58203/
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Institution: Universiti Sains Malaysia
Language: English

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