Development of a dynamic wind tunnel rig for aircraft pure pitching motion

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Development of a dynamic wind tunnel rig for aircraft pure pitching motion

This paper presents the design, fabrication and testing of a dynamic wind tunnel test rig that is used in conjunction with aircraft dynamics theory in estimating aerodynamics stability derivatives. The value of and can be obtained from free oscillation theory of pure pitching motion. The rig compris...

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Bibliographic Details
Main Authors:	Mansor, Shuhaimi, Ishak, Iskandar Shah, Ong, Meng Wei, Fahrurazi, Istas
Format:	Article
Language:	English
Published:	Faculty of Mechanical Engineering 2000
Subjects:	TJ Mechanical engineering and machinery TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.utm.my/8314/ http://eprints.utm.my/8314/1/ShuhaimiMansor2000_DevelopmentofaDynamicWind.pdf

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