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RISEffects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and analytical study has been performed on the effect of Reynolds number and free-stream turbulence on boundary layer transition location on the suction surface of a controlled ...
Advanced 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 ...
3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and numerical study of the transonic flow through a linear compressor cascade with endwalls was conducted. The cascade with a low aspect ratio of 1.34 was tested at an inlet ...
Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Modern methods for axial compressor design are capable of shaping the blade surfaces in a three-dimensional way. Linking these methods with automated optimization techniques provides a major ...