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Comprehensive Experimental Assessment of Unsteady Pressure and Heat Flux in a Small-Core Turbine Over-Tip Shroud
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: For novel high-speed small core turbines, with tip clearance below 0.5 mm, even small blade-to-blade tip clearance variation is significant. The assessment of these complex flows is pertinent to the design of the next ...
Design, Optimization, and Analysis of Supersonic Radial Turbines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: New compact engine architectures such as pressure gain combustion require ad hoc turbomachinery to ensure an adequate range of operation with high performance. A critical factor for supersonic turbines is to ensure the ...