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Proceedings Papers

Design, Optimization, and Analysis of a High-Turning Transonic Tandem Compressor Cascade

Proc. ASME. GT1997, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A067, June 2–5, 1997

Publisher: American Society of Mechanical Engineers

Paper No: 97-GT-412

https://doi.org/10.1115/97-GT-412

View Paper titled, Design, Optimization, and Analysis of a High-Turning Transonic Tandem Compressor Cascade

Topics: Cascades (Fluid dynamics), Compressors, Design, Optimization, Turning, Blades, Flow (Dynamics), Flow turning, Pressure, Mach number

Proceedings Papers

Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

Heinz-Adolf Schreiber, Wolfgang Steinert, Bernhard Küsters

Proc. ASME. GT2000, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A068, May 8–11, 2000

Publisher: American Society of Mechanical Engineers

Paper No: 2000-GT-0263

https://doi.org/10.1115/2000-GT-0263

View Paper titled, Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

Topics: Boundary layers, Cascades (Fluid dynamics), Compressors, Reynolds number, Turbulence, Blades, Chords (Trusses), Airfoils, Bubbles, Coatings

Proceedings Papers

3D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Anton Weber, Heinz-Adolf Schreiber, Reinhold Fuchs, Wolfgang Steinert

Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A041, June 4–7, 2001

Publisher: American Society of Mechanical Engineers

Paper No: 2001-GT-0345

https://doi.org/10.1115/2001-GT-0345

View Paper titled, 3D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Topics: Cascades (Fluid dynamics), Compressors, Corners (Structural elements), Shock (Mechanics), Transonic flow, Flow (Dynamics), Blades, Pressure, Vortices, Wakes

Journal Articles

Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Alexander Hergt, Christian Dorfner, Wolfgang Steinert, Eberhard Nicke, Heinz-Adolf Schreiber

Publisher: ASME

J. Turbomach. April 2011, 133(2): 021027.

https://doi.org/10.1115/1.4001224

Published Online: October 27, 2010

View Article titled, Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Topics: Cascades (Fluid dynamics), Flow (Dynamics), Blades, Compressors, Pressure

Proceedings Papers

Advanced Non-Axisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Alexander Hergt, Christian Dorfner, Wolfgang Steinert, Eberhard Nicke, Heinz-Adolf Schreiber

Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 121-131, June 8–12, 2009

Publisher: American Society of Mechanical Engineers

Paper No: GT2009-59384

https://doi.org/10.1115/GT2009-59384

View Paper titled, Advanced Non-Axisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Topics: Cascades (Fluid dynamics), Compressors, Design, Flow (Dynamics), Blades, Boundary layers, Vortices, Computer simulation, Corners (Structural elements), Flow simulation

Proceedings Papers

Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition: Part 2 — Experimental and Numerical Analysis

Heinz-Adolf Schreiber, Wolfgang Steinert, Toyotaka Sonoda, Toshiyuki Arima

Proc. ASME. GT2003, Volume 6: Turbo Expo 2003, Parts A and B, 451-463, June 16–19, 2003

Publisher: American Society of Mechanical Engineers

Paper No: GT2003-38477

https://doi.org/10.1115/GT2003-38477

View Paper titled, Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition: Part 2 — Experimental and Numerical Analysis

Topics: Airfoils, Compressors, Numerical analysis, Reynolds number, Turning, Design, Boundary layers, Cascades (Fluid dynamics), Diffusion (Physics), Flow (Dynamics)

Journal Articles

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 ]

Heinz-Adolf Schreiber, Wolfgang Steinert, Toyotaka Sonoda, Toshiyuki Arima

Publisher: ASME

J. Turbomach. July 2005, 127(3): 646.

https://doi.org/10.1115/1.1997107

Published Online: July 1, 2005

View Article titled, 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 ]

Topics: Airfoils, Compressors, Numerical analysis, Reynolds number, Turbomachinery, Turning

Journal Articles

Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition—Part II: Experimental and Numerical Analysis

Heinz-Adolf Schreiber, Wolfgang Steinert, Toyotaka Sonoda, Toshiyuki Arima

Publisher: ASME

J. Turbomach. October 2004, 126(4): 482–492.

https://doi.org/10.1115/1.1737781

Published Online: December 29, 2004

View Article titled, Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition—Part II: Experimental and Numerical Analysis

Topics: Blades, Boundary layers, Design, Reynolds number, Mach number, Cascades (Fluid dynamics), Separation (Technology), Flow (Dynamics), Compressors, Suction

Journal Articles

3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Anton Weber, Heinz-Adolf Schreiber, Reinhold Fuchs, Wolfgang Steinert

Publisher: ASME

J. Turbomach. July 2002, 124(3): 358–366.

https://doi.org/10.1115/1.1460913

Published Online: July 10, 2002

View Article titled, 3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Topics: Blades, Cascades (Fluid dynamics), Compressors, Corners (Structural elements), Flow (Dynamics), Mach number, Pressure, Shock (Mechanics), Simulation, Transonic flow

Journal Articles

Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

Heinz-Adolf Schreiber, Wolfgang Steinert, Bernhard Ku¨sters

Publisher: ASME

J. Turbomach. January 2002, 124(1): 1–9.

https://doi.org/10.1115/1.1413471

Published Online: February 1, 2000

View Article titled, Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Chords (Trusses), Compressors, Liquid crystals, Reynolds number, Suction, Surface roughness, Turbulence

Journal citation

NARROW

Design, Optimization, and Analysis of a High-Turning Transonic Tandem Compressor Cascade

Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

3D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Advanced Non-Axisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator—Part II: Experimental and Numerical Cascade Investigation

Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition: Part 2 — Experimental and Numerical Analysis

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 ]

Advanced High-Turning Compressor Airfoils for Low Reynolds Number Condition—Part II: Experimental and Numerical Analysis

3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall

Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade

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