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T3.4: Turbomachinery noise
Monday, 28/Aug/2017: 13:40 - 15:00 Session Chair: Xun Huang
Location: S423 S423, Level 4, HKCEC
Compressive sensing bases spinning mode detection for aeroengine noise
1Peking University, Beijing, China.; 2Hong Kong University of Science and Technology, Hong Kong, China.
A modified Fourier solution for the Flapwise bending vibration analysis of rotating beams with elastic boundary conditions
Harbin Engineering University, China, People's Republic of
Tonal noise characteristics of mulit-rotor micro aerial vehicles
Hong Kong University of Science and Technology, Hong Kong S.A.R. (China)
TURBOMACHINERY TONAL NOISE CFD-CAA MODELING IN PRESENCE OF SAS COMPLEX ACOUSTIC IMPEDANCE BOUNDARIES
1Moscow Aviation Institute, Russian Federation; 2Tesis Ltd., Russian Federation