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RISUnsteady Boundary-Layer Transition in Flow Periodically Disturbed by Wakes
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Boundary layers on turbomachinery blades develop in a flow that is periodically disturbed by the wakes of upstream blade cascades. These wakes have a significant effect upon laminar-turbulent ...
Discussion: “Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion” (Funazaki, K., 1996, ASME J. Turbomach., 118, pp. 337–344)
Publisher: The American Society of Mechanical Engineers (ASME)
Improved Compressor Exit Diffuser for an Industrial Gas Turbine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Cycle studies carried out for the medium pressure ratio gas turbine THM 1304 of 10 MW power output manufactured by MAN Turbomaschinen AG GHH BORSIG predicted that the overall efficiency of ...