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Proceedings Papers

Experimental Study of Three-Dimensional Flow in an Axial Compressor Stage

Vaclav Cyrus
Proc. ASME. GT1986, Volume 1: Turbomachinery, V001T01A047, June 8–12, 1986
Publisher: American Society of Mechanical Engineers
Paper No: 86-GT-118
https://doi.org/10.1115/86-GT-118
View Paper titled, Experimental Study of Three-Dimensional Flow in an Axial Compressor Stage
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Topics: Compressors, Flow (Dynamics), Blades, Rotors, Stators, Diffusion (Physics), Pressure, Probes
Proceedings Papers

The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade

Václav Cyrus
Proc. ASME. GT1988, Volume 1: Turbomachinery, V001T01A096, June 6–9, 1988
Publisher: American Society of Mechanical Engineers
Paper No: 88-GT-269
https://doi.org/10.1115/88-GT-269
View Paper titled, The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
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Topics: Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Reynolds number, Blades, Tunnels
Proceedings Papers

The Turbine Regime of a Rear Axial Compressor Stage

Václav Cyrus
Proc. ASME. GT1990, Volume 1: Turbomachinery, V001T01A025, June 11–14, 1990
Publisher: American Society of Mechanical Engineers
Paper No: 90-GT-074
https://doi.org/10.1115/90-GT-074
View Paper titled, The Turbine Regime of a Rear Axial Compressor Stage
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Topics: Compressors, Turbines, Flow (Dynamics), Design, Blades, Pressure, Probes, Rotors, Stators
Proceedings Papers

Prediction of Secondary Losses in Axial Compressors

Václav Cyrus
Proc. ASME. GT1992, Volume 1: Turbomachinery, V001T01A098, June 1–4, 1992
Publisher: American Society of Mechanical Engineers
Paper No: 92-GT-288
https://doi.org/10.1115/92-GT-288
View Paper titled, Prediction of Secondary Losses in Axial Compressors
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Topics: Compressors, Blades, Clearances (Engineering), Computation, Design
Proceedings Papers

Separated Flows in Axial Flow Compressor With Variable Stator Vanes at Positive Incidence Angles

Vaclav Cyrus
Proc. ASME. GT1994, Volume 1: Turbomachinery, V001T01A151, June 13–16, 1994
Publisher: American Society of Mechanical Engineers
Paper No: 94-GT-480
https://doi.org/10.1115/94-GT-480
View Paper titled, Separated Flows in Axial Flow Compressor With Variable Stator Vanes at Positive Incidence Angles
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Topics: Axial flow, Flow (Dynamics), Stators, Blades, Compressors, Diffusion (Physics), Rotors, Pressure, Probes
Proceedings Papers

Aerodynamic Performance of Rear Axial Compressor Stage With Annular Diffuser and Outlet Chamber

Václav Cyrus
Proc. ASME. GT1996, Volume 1: Turbomachinery, V001T01A068, June 10–13, 1996
Publisher: American Society of Mechanical Engineers
Paper No: 96-GT-238
https://doi.org/10.1115/96-GT-238
View Paper titled, Aerodynamic Performance of Rear Axial Compressor Stage With Annular Diffuser and Outlet Chamber
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Topics: Compressors, Diffusers, Guide vanes, Annulus, Blades, Cascades (Fluid dynamics), Design, Rotors, Stators
Proceedings Papers

The Influence of Outlet Stator Part Surface Roughness on the Performance of a Very Low Flow Coefficient Centrifugal Compressor Stage

Jan Paroubek, Václav Cyrus, Jiři Kynčl
Proc. ASME. GT1996, Volume 1: Turbomachinery, V001T01A063, June 10–13, 1996
Publisher: American Society of Mechanical Engineers
Paper No: 96-GT-179
https://doi.org/10.1115/96-GT-179
View Paper titled, The Influence of Outlet Stator Part Surface Roughness on the Performance of a Very Low Flow Coefficient Centrifugal Compressor Stage
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Topics: Compressors, Flow (Dynamics), Stators, Surface roughness, Surface quality, Vaneless diffusers, Design, Dynamic stability, Mach number, Pressure
Proceedings Papers

Aerodynamic Performance of an Axial Compressor Stage With Variable Rotor Blades and Variable Inlet Guide Vanes

Václav Cyrus
Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A044, June 2–5, 1998
Publisher: American Society of Mechanical Engineers
Paper No: 98-GT-151
https://doi.org/10.1115/98-GT-151
View Paper titled, Aerodynamic Performance of an Axial Compressor Stage With Variable Rotor Blades and Variable Inlet Guide Vanes
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Topics: Blades, Compressors, Inlet guide vanes, Rotors, Axial flow, Flow (Dynamics), Pressure, Stators, Design, Flow separation
Proceedings Papers

An Experimental Study of Stall in Four Axial Compressor Stages

Vaclav Cyrus
Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A073, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0504
https://doi.org/10.1115/2000-GT-0504
View Paper titled, An Experimental Study of Stall in Four Axial Compressor Stages
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Topics: Compressors, Flow (Dynamics), Blades, Stability, Rotors, Inlet guide vanes, Stators, Clearances (Engineering), Corners (Structural elements), Design
Proceedings Papers

Reversing of Axial Flow Fans for Ventilation

Vaclav Cyrus, Jiri Pelnar, Jan Cyrus
Proc. ASME. GT2011, Volume 4: Cycle Innovations; Fans and Blowers; Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Oil and Gas Applications, 471-482, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-46062
https://doi.org/10.1115/GT2011-46062
View Paper titled, Reversing of Axial Flow Fans for Ventilation
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Topics: Axial flow, Fans, Ventilation, Flow (Dynamics), Blades, Design, Pressure, Rotation, Aerodynamics, Compressors
Journal Articles

Numerical Simulation of the Flow Pulsations Origin in Cascades of the Rear Blade Rows in a Gas Turbine Axial Compressor Using Low Calorific Fuel

Vaclav Cyrus, Jiri Polansky
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2010, 132(3): 031012.
https://doi.org/10.1115/1.3153306
Published Online: March 25, 2010
View Article titled, Numerical Simulation of the Flow Pulsations Origin in Cascades of the Rear Blade Rows in a Gas Turbine Axial Compressor Using Low Calorific Fuel
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Topics: Blades, Cascades (Fluid dynamics), Compressors, Flow (Dynamics), Flow simulation, Gas turbines, Rotors, Stators, Vortices, Fuels
Proceedings Papers

Numerical Simulation of the Flow Pulsations Origin in Cascades of the Rear Blade Rows in a Gas Turbine Axial Compressor Using Low Calorific Fuel

Vaclav Cyrus, Jiri Polansky
Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 519-531, June 9–13, 2008
Publisher: American Society of Mechanical Engineers
Paper No: GT2008-50966
https://doi.org/10.1115/GT2008-50966
View Paper titled, Numerical Simulation of the Flow Pulsations Origin in Cascades of the Rear Blade Rows in a Gas Turbine Axial Compressor Using Low Calorific Fuel
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Topics: Blades, Compressors, Computer simulation, Flow (Dynamics), Fuels, Gas turbines, Stators, Cascades (Fluid dynamics), Rotors, Flow simulation