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H. P. Pirker
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Proceedings Papers

Operational Behavior of a Complex Transonic Test Turbine Facility

F. Neumayer, G. Kulhanek, H.-P. Pirker, H. Jericha, A. Seyr, W. Sanz
Proc. ASME. GT2001, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A073, June 4–7, 2001
Paper No: 2001-GT-0489
DOI: https://doi.org/10.1115/2001-GT-0489
View Paper titled, Operational Behavior of a Complex Transonic Test Turbine Facility
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Topics: Turbines, Compressors, Brakes, Pressure, Design, Engineers, Engines, Exhaust systems, Flow (Dynamics), Suction
Journal Articles

The Effect of Rotor Tip Clearance Size onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage

A. Marn, E. Göttlich, F. Malzacher, H. P. Pirker
Journal: Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach. September 2012, 134(5): 051019.
DOI: https://doi.org/10.1115/1.4004446
Published Online: May 11, 2012
View Article titled, The Effect of Rotor Tip Clearance Size onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage
Click here to open pdf in another window PDF for The Effect of Rotor Tip Clearance Size onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage
Topics: Ducts, Flow (Dynamics), Pressure, Rotors, Turbines, Clearances (Engineering), Boundary layers, Mach number, Probes, Flow visualization
Proceedings Papers

The Effect of Rotor Tip Clearance Size Onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage

A. Marn, E. Go¨ttlich, F. Malzacher, H. P. Pirker
Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 1089-1103, June 8–12, 2009
Paper No: GT2009-59934
DOI: https://doi.org/10.1115/GT2009-59934
View Paper titled, The Effect of Rotor Tip Clearance Size Onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage
Click here to open pdf in another window PDF for The Effect of Rotor Tip Clearance Size Onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage
Topics: Clearances (Engineering), Ducts, Flow (Dynamics), Rotors, Turbines, Pressure, Separation (Technology), Aircraft engines, Blades, Diffusion (Physics)
Proceedings Papers

Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept

A. Marn, E. Go¨ttlich, D. Cadrecha, H. P. Pirker
Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1041-1051, June 9–13, 2008
Paper No: GT2008-50269
DOI: https://doi.org/10.1115/GT2008-50269
View Paper titled, Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept
Click here to open pdf in another window PDF for Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept
Topics: Ducts, Turbines, Flow (Dynamics), Design, Engines, Struts (Engineering), Weight (Mass), Bearings, Chords (Trusses), Pressure
Journal Articles

Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept

A. Marn, E. Göttlich, D. Cadrecha, H. P. Pirker
Journal: Journal of Turbomachinery
Article Type: Research Papers
J. Turbomach. October 2009, 131(4): 041014.
DOI: https://doi.org/10.1115/1.3070578
Published Online: July 6, 2009
View Article titled, Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept
Click here to open pdf in another window PDF for Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept
Topics: Design, Ducts, Flow (Dynamics), Pressure, Struts (Engineering), Turbines, Mach number, Probes, Blades, Yaw
Proceedings Papers

The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part I — Time-Averaged Results

A. Marn, E. Go¨ttlich, R. Pecnik, F. J. Malzacher, O. Schennach, H. P. Pirker
Proc. ASME. GT2007, Volume 6: Turbo Expo 2007, Parts A and B, 575-585, May 14–17, 2007
Paper No: GT2007-27405
DOI: https://doi.org/10.1115/GT2007-27405
View Paper titled, The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part I — Time-Averaged Results
Click here to open pdf in another window PDF for The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part I — Time-Averaged Results
Topics: Blades, Ducts, Flow (Dynamics), Turbines, Pressure, Diffusion (Physics), Aircraft engines, Probes, Boundary layers, Design
Proceedings Papers

The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part II — Time-Resolved Results and Surface Flow

E. Go¨ttlich, A. Marn, R. Pecnik, F. J. Malzacher, O. Schennach, H. P. Pirker
Proc. ASME. GT2007, Volume 6: Turbo Expo 2007, Parts A and B, 843-853, May 14–17, 2007
Paper No: GT2007-28069
DOI: https://doi.org/10.1115/GT2007-28069
View Paper titled, The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part II — Time-Resolved Results and Surface Flow
Click here to open pdf in another window PDF for The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-Shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage: Part II — Time-Resolved Results and Surface Flow
Topics: Blades, Ducts, Flow (Dynamics), Turbines, Pressure, Diffusion (Physics), Aircraft engines, Aerodynamics, Boundary layers, Computer simulation