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A Transonic Axial Compressor Facility for Fundamental Research and Flow Control Development
Design of a Transonic Research Turbine Facility
Trailing Edge Flow Physics and Acoustics
Radiated Sound And Turbulent Motions In A Blunt Trailing Edge Flow Field
Turbulent Boundary Layer To Single-Stream Shear Layer: The Transition Region
Vorticity Spectra In High Reynolds Number Anisotropic Turbulence
Near Surface Turbulence in A Smooth Wall Atmospheric Boundary Layer
Turbine Tip Clearance Flow Control Using Plasma Actuators
Experimental Investigation of a Blunt Trailing Edge Flow Field with Application to Sound Generation