Unsteady Pressure Measurement Of NACA 0018 Undergoing Pure Pitching Motion At Different Pitch Amplitudes

Tong, Chee Kent (2017) Unsteady Pressure Measurement Of NACA 0018 Undergoing Pure Pitching Motion At Different Pitch Amplitudes. Project Report. Universiti Sains Malaysia, Pusat Pengajian Kejuruteraan Aeroangkasa. (Submitted)

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Abstract

An experimental investigation of the unsteady pressure measurement of a 2D NACA 0018 airfoil oscillating in pitch motion was performed by using pressure transducers at open-circuit wind tunnel. In the case of study, the wind tunnel testing was conducted in low flight regimes (

Item Type:	Monograph (Project Report)
Subjects:	T Technology
Divisions:	Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Aeroangkasa (School of Aerospace Engineering) > Monograph
Depositing User:	Mr Mohamed Yunus Mat Yusof
Date Deposited:	01 Mar 2022 05:10
Last Modified:	01 Mar 2022 05:10
URI:	http://eprints.usm.my/id/eprint/51763

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