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RISAdvanced High-Turning Compressor Airfoils for Low Reynolds Number Condition—Part II: Experimental and Numerical Analysis
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Part I of this paper describes the design and optimization of two high turning subsonic compressor cascades operating as an outlet guide vane (OGV) behind a single stage low pressure turbine ...
Erratum: “Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition—Part II: Experimental and Numerical Analysis” [Journal of Turbomachinery, 2004, 126(4), pp. 482–492]
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Page 483, left column, 19 lines from the top, “Fig. 1 (left)” should be replaced by “Fig. 5 (left)”.Page 483, left column, 21 lines from the top, “see Fig. 2” should be replaced by “see ...
Effect of End Wall Contouring on Performance of Ultra-Low Aspect Ratio Transonic Turbine Inlet Guide Vanes
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In our previous work on ultralow-aspect ratio transonic turbine inlet guide vanes (IGVs) for a small turbofan engine (, 2005, “ Three Dimensional Aerodynamic Optimization for an Ultra-Low Aspect ...
A Study of Advanced High-Loaded Transonic Turbine Airfoils
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The development of high-performance turbine airfoils has been investigated under the condition of a supersonic exit Mach number. In order to obtain a new aerodynamic design concept for a ...
Microscale Radial-Flow Compressor Impeller Made of Silicon Nitride: Manufacturing and Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A microscale, high-speed compressor impeller (12 mm diameter, 800,000 rpm) was tested for feasibility in regard to aerodynamic performance. The compressor was designed for application in a ...