Highly versatile with extensive past experience in supporting aviation industry. Proven ability to resolve significant noise / acoustic challenges. Strong in analytical, experimental, and root-cause analysis. Collaborative in team work, and capable to resolve problem independently.Produced 9 acoustic patents for low noise features, covering various type of aero-engine noise, such as butterfly valve noise, fan-stator interaction noise, bypass-duct fan noise, exhaust jet noise, and vortex whistle noise (search key words: Man-Chun Tse AND patents).EXPERIENCE & EXPERTISE:Acoustics:• 30+ year’s practical experience.• Solid knowledge of acoustic theories in many aspects: aero-engine noise sources, flow-induced, duct, nonlinear, architectural, structural, ocean, sound quality (psychoacoustics), outdoor sound propagation, digital signal processing.Aerodynamics: • 5+ year’s practical experience (including engine icing tests) in: flow and pressure measurements, subsonic wind tunnel, intake & exhaust rigs, ducts and valves.• Solid knowledge of aerodynamic theories: compressible, incompressible, potential, turbulent flows, boundary layer, thin airfoil theory.Worked at Pratt & Whitney Canada for 40+ years in R&D (acoustic + aerodynamics), taught acoustic courses.Reviewed conference papers (acoustics) for ASME Turbomachinery Conference, 2010 to 2013 inclusively.PUBLICATION AND PRESENTATION:• Flow past a thin inflated lenticular aerofoil, by B.G. Newman, M-C. Tse, J. Fluid Mech., 1980, vol. 100.• Thin Un-cambered Aerofoil with Leading-Edge Separation Bubble, by B.G. Newman, M-C. Tse, Proc. 10th Australasian Fluid Mechanics Conf., 1989, vol. I.• Incompressible flow past a flat plate aerofoil with leading edge separation bubble, by B.G. Newman, M-C. Tse, The Aeronautical Journal, Feb/1992, vol. 96, No. 952.• Vortex-Whistle in Radial Intake, by M-C. Tse, RTO-AVT-110, Paper #22, NATO Symposium at Prague, Oct/2004.