Unsteady Pressure Measurement Of NACA 0018 Undergoing Pure Pitching Motion At Different Pitch Amplitudes
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 (
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| Format: | Monograph |
| Language: | English |
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Universiti Sains Malaysia
2017
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| Online Access: | http://eprints.usm.my/51763/1/Unsteady%20Pressure%20Measurement%20Of%20NACA%200018%20%20Undergoing%20Pure%20Pitching%20Motion%20%20At%20Different%20Pitch%20Amplitudes_Tong%20Chee%20Kent_A2_2017.pdf |