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Douglas C. Rabe
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Proceedings Papers

A Methodology for Variable Geometry Optimization of Multistage Axial Compressors

M. Eric Lyall, Fred J. Eisert, Douglas C. Rabe, Patrick M. Fleisher
Proc. ASME. GT2017, Volume 2A: Turbomachinery, V02AT39A037, June 26–30, 2017
Publisher: American Society of Mechanical Engineers
Paper No: GT2017-64874
https://doi.org/10.1115/GT2017-64874
View Paper titled, A Methodology for Variable Geometry Optimization of Multistage Axial Compressors
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Topics: Compressors, Geometry, Optimization, Experimental design, Flow (Dynamics), Pressure, Design, Machinery, Modeling, Response surface methodology
Proceedings Papers

Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor

Chunill Hah, Douglas C. Rabe, Thomas J. Sullivan, Aspi R. Wadia
Proc. ASME. GT1996, Volume 1: Turbomachinery, V001T01A135, June 10–13, 1996
Publisher: American Society of Mechanical Engineers
Paper No: 96-GT-547
https://doi.org/10.1115/96-GT-547
View Paper titled, Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor
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Topics: Compressors, Flow (Dynamics), Rotors, Blades, Pressure, Shock (Mechanics), Boundary layers, Viscous flow, Boundary-value problems, Chords (Trusses)
Proceedings Papers

Inlet Distortion Generated Forced Response of a Low Aspect Ratio Transonic Fan

Steven R. Manwaring, Douglas C. Rabe, Christopher B. Lorence, Aspi R. Wadia
Proc. ASME. GT1996, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General, V005T14A039, June 10–13, 1996
Publisher: American Society of Mechanical Engineers
Paper No: 96-GT-376
https://doi.org/10.1115/96-GT-376
View Paper titled, Inlet Distortion Generated Forced Response of a Low Aspect Ratio Transonic Fan
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Topics: Acoustics, Aerodynamics, Airfoils, Blades, Boundary layers, Flow (Dynamics), Pressure, Pressure transducers, Resonance, Shock (Mechanics)
Proceedings Papers

Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor

Donald W. Thompson, Paul I. King, Douglas C. Rabe
Proc. ASME. GT1997, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A002, June 2–5, 1997
Publisher: American Society of Mechanical Engineers
Paper No: 97-GT-007
https://doi.org/10.1115/97-GT-007
View Paper titled, Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor
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Topics: Axial flow, Compressors, Rotors, Clearances (Engineering), Flow (Dynamics), Design, Engineers, Inlet guide vanes, Pressure
Proceedings Papers

Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor

Donald W. Thompson, Paul I. King, Chunill Hah, Douglas C. Rabe
Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A026, June 2–5, 1998
Publisher: American Society of Mechanical Engineers
Paper No: 98-GT-090
https://doi.org/10.1115/98-GT-090
View Paper titled, Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor
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Topics: Axial flow, Compressors, Rotors, Clearances (Engineering), Flow (Dynamics), Geometry, Computational fluid dynamics, Design, Engineers, Inlet guide vanes
Proceedings Papers

The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

Kelly R. Navarra, Douglas C. Rabe, Larry P. Goss
Proc. ASME. GT2000, Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education, V004T04A031, May 8–11, 2000
Publisher: American Society of Mechanical Engineers
Paper No: 2000-GT-0614
https://doi.org/10.1115/2000-GT-0614
View Paper titled, The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor
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Topics: Compressors, Paints, Pressure, Temperature, Rotors, Suction, Aerospace industry, Coating processes, Coatings, Design
Journal Articles

Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part I: Development of Prediction Methodology

Darius D. Sanders, Walter F. O’Brien, Rolf Sondergaard, Marc D. Polanka, Douglas C. Rabe
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2011, 133(3): 031011.
https://doi.org/10.1115/1.4001230
Published Online: November 15, 2010
View Article titled, Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part I: Development of Prediction Methodology
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Topics: Airfoils, Blades, Boundary layers, Computational fluid dynamics, Flow (Dynamics), Pressure, Reynolds number, Separation (Technology), Turbulence, Simulation
Journal Articles

Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part II: The Application to a Highly Separated Turbine Blade Cascade Geometry

Darius D. Sanders, Walter F. O’Brien, Rolf Sondergaard, Marc D. Polanka, Douglas C. Rabe
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2011, 133(3): 031012.
https://doi.org/10.1115/1.4001231
Published Online: November 15, 2010
View Article titled, Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part II: The Application to a Highly Separated Turbine Blade Cascade Geometry
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Topics: Airfoils, Blades, Boundary layers, Computational fluid dynamics, Flow (Dynamics), Pressure, Reynolds number, Separation (Technology), Turbulence, Geometry
Proceedings Papers

Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers

Darius D. Sanders, Walter F. O’Brien, Rolf Sondergaard, Marc D. Polanka, Douglas C. Rabe
Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1053-1068, June 9–13, 2008
Publisher: American Society of Mechanical Engineers
Paper No: GT2008-50283
https://doi.org/10.1115/GT2008-50283
View Paper titled, Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers
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Topics: Flow (Dynamics), Reynolds number, Separation (Technology), Turbine blades, Turbulence, Boundary layers, Computational fluid dynamics, Turbines, Blades, Cascades (Fluid dynamics)
Proceedings Papers

Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor

Chunill Hah, Douglas C. Rabe, Aspi R. Wadia
Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 545-555, June 14–17, 2004
Publisher: American Society of Mechanical Engineers
Paper No: GT2004-53867
https://doi.org/10.1115/GT2004-53867
View Paper titled, Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor
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Topics: Compressors, Leakage, Rotors, Shock (Mechanics), Stall inception, Vortices, Clearances (Engineering), Flow (Dynamics), Blades, Boundary layers
Journal Articles

The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

Kelly R. Navarra, Douglas C. Rabe, Sergey D. Fonov, Larry P. Goss, Chunill Hah
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. October 2001, 123(4): 823–829.
https://doi.org/10.1115/1.1400116
Published Online: February 1, 2000
View Article titled, The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor
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Topics: Compressors, Paints, Pressure, Temperature, Computational fluid dynamics, Pressure measurement, Blades