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Proceedings Papers

Comparison of Two and Three Dimensional Flow Computations With Laser Anemometer Measurements in a Transonic Compressor Rotor

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R. V. Chima, A. J. Strazisar
Proc. ASME. GT1982, Volume 1: Turbomachinery, V001T01A095, April 18–22, 1982
Publisher: American Society of Mechanical Engineers
Paper No: 82-GT-302
https://doi.org/10.1115/82-GT-302
View Paper titled, Comparison of Two and Three Dimensional Flow Computations With Laser Anemometer Measurements in a Transonic Compressor Rotor
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Topics: Compressors, Computation, Flow (Dynamics), Lasers, Rotors, Blades, Design, Mach number, Pressure, Waves
Proceedings Papers

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part I — Experimental Study

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J. Lepicovsky, E. R. McFarland, R. V. Chima, J. R. Wood
Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A097, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0572
https://doi.org/10.1115/2000-GT-0572
View Paper titled, On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part I — Experimental Study
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Topics: Cascades (Fluid dynamics), Flutter (Aerodynamics), NASA, Blades, Flow (Dynamics), Boundary layers, Stress, Tunnels, Data acquisition, Geometry
Proceedings Papers

On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part II — Numerical Study

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R. V. Chima, E. R. McFarland, J. R. Wood, J. Lepicovsky
Proc. ASME. GT2000, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A098, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0573
https://doi.org/10.1115/2000-GT-0573
View Paper titled, On Flowfield Periodicity in the NASA Transonic Flutter Cascade: Part II — Numerical Study
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Topics: Cascades (Fluid dynamics), Flutter (Aerodynamics), NASA, Blades, Computational fluid dynamics, Boundary layers, Flow (Dynamics), Numerical analysis, Paints, Pressure
Proceedings Papers

Computational Modeling of Vortex Generators for Turbomachinery

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R. V. Chima
Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 1229-1238, June 3–6, 2002
Publisher: American Society of Mechanical Engineers
Paper No: GT2002-30677
https://doi.org/10.1115/GT2002-30677
View Paper titled, Computational Modeling of Vortex Generators for Turbomachinery
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Topics: Computer simulation, Generators, Turbomachinery, Vortices, Stators, Compressors, Rotors, Engines, Flow (Dynamics), NASA
Proceedings Papers

A Three-Dimensional Unsteady CFD Model of Compressor Stability

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R. V. Chima
Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 1157-1168, May 8–11, 2006
Publisher: American Society of Mechanical Engineers
Paper No: GT2006-90040
https://doi.org/10.1115/GT2006-90040
View Paper titled, A Three-Dimensional Unsteady CFD Model of Compressor Stability
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Topics: Compressors, Computational fluid dynamics, Stability, Blades, Pressure, Annulus, NASA, Turbomachinery
Journal Articles

On Flowfield Periodicity in the NASA Transonic Flutter Cascade

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J. Lepicovsky, R. V. Chima, E. R. McFarland, J. R. Wood
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2001, 123(3): 501–509.
https://doi.org/10.1115/1.1378300
Published Online: February 1, 2000
View Articletitled, On Flowfield Periodicity in the NASA Transonic Flutter Cascade
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Topics: Blades, Cascades (Fluid dynamics), Flow (Dynamics), Pressure, Flutter (Aerodynamics), Boundary layers
Journal Articles

Calculation of Tip Clearance Effects in a Transonic Compressor Rotor

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R. V. Chima
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 1998, 120(1): 131–140.
https://doi.org/10.1115/1.2841374
Published Online: January 1, 1998
View Articletitled, Calculation of Tip Clearance Effects in a Transonic Compressor Rotor
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Topics: Clearances (Engineering), Compressors, Rotors, Lasers, Boundary layers, Computation, Flow (Dynamics), NASA, Probes, Separation (Technology)
Journal Articles

The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor

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K. L. Suder, R. V. Chima, A. J. Strazisar, W. B. Roberts
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 1995, 117(4): 491–505.
https://doi.org/10.1115/1.2836561
Published Online: October 1, 1995
View Articletitled, The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor
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Topics: Compressors, Rotors, Surface roughness, Coatings, Coating processes, Blades, Design, Finishes, Airfoils, Boundary layers
Journal Articles

Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor

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J. R. Wood, J. F. Schmidt, R. J. Steinke, R. V. Chima, W. G. Kunik
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 1988, 110(2): 270–279.
https://doi.org/10.1115/1.3262191
Published Online: April 1, 1988
View Articletitled, Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor
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Topics: Design, Rotors, Blades, Mach number, Nozzles, Boundary layers, Flow (Dynamics), Shapes, Axial flow, Databases
Journal Articles

Comparison of Two- and Three-Dimensional Flow Computations With Laser Anemometer Measurements in a Transonic Compressor Rotor

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R. V. Chima, A. J. Strazisar
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. July 1983, 105(3): 596–605.
https://doi.org/10.1115/1.3227459
Published Online: July 1, 1983
View Articletitled, Comparison of Two- and Three-Dimensional Flow Computations With Laser Anemometer Measurements in a Transonic Compressor Rotor
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Topics: Compressors, Computation, Flow (Dynamics), Lasers, Rotors, Blades, Design, Mach number, Pressure, Waves