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M. Hoeger
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Proceedings Papers

The Effect of Reynolds Number and Velocity Distribution on LP Turbine Cascade Performance

D. J. Patterson, M. Hoeger
Proc. ASME. GT1986, Volume 1: Turbomachinery, V001T01A113, June 8–12, 1986
Publisher: American Society of Mechanical Engineers
Paper No: 86-GT-271
https://doi.org/10.1115/86-GT-271
View Paper titled, The Effect of Reynolds Number and Velocity Distribution on LP Turbine Cascade Performance
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Topics: Cascades (Fluid dynamics), Reynolds number, Turbines, Pressure, Design, Flow (Dynamics), Boundary layers, Deflection, Mach number, Nozzle guide vanes
Proceedings Papers

Prediction of 2D Viscous Transonic Flow in Compressor Cascades Using a Semi-Empirical Shock/Boundary-Layer Interaction Method

M. Hoeger, K. D. Broichhausen
Proc. ASME. GT1992, Volume 1: Turbomachinery, V001T01A087, June 1–4, 1992
Publisher: American Society of Mechanical Engineers
Paper No: 92-GT-277
https://doi.org/10.1115/92-GT-277
View Paper titled, Prediction of 2D Viscous Transonic Flow in Compressor Cascades Using a Semi-Empirical Shock/Boundary-Layer Interaction Method
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Topics: Boundary layers, Compressors, Shock (Mechanics), Transonic flow, Flow (Dynamics), Computational methods, Design, Engineers, Mach number, Turbulence
Proceedings Papers

Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage

M. Hoeger, G. Fritsch, D. Bauer
Proc. ASME. GT1998, Volume 1: Turbomachinery, V001T01A073, June 2–5, 1998
Publisher: American Society of Mechanical Engineers
Paper No: 98-GT-261
https://doi.org/10.1115/98-GT-261
View Paper titled, Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage
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Topics: Computer simulation, Leakage, Shock (Mechanics), Vortices, Simulation, Flow (Dynamics), Blades, Compressors, Displacement, Instrumentation
Proceedings Papers

A Correlation for Tip Leakage Blockage in Compressor Blade Passages

M. Hoeger, M. Lahmer, M. Dupslaff, G. Fritsch
Proc. ASME. GT1999, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A055, June 7–10, 1999
Publisher: American Society of Mechanical Engineers
Paper No: 99-GT-388
https://doi.org/10.1115/99-GT-388
View Paper titled, A Correlation for Tip Leakage Blockage in Compressor Blade Passages
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Topics: Blades, Compressors, Leakage, Displacement, Flow (Dynamics), Chords (Trusses), Mach number, Navier-Stokes equations
Proceedings Papers

Comparison of the Experimental Results Between a 2D EGV Cascade Test and a Rig Test Under Engine Representative Conditions

F. Schönleitner, H. Koch, T. Selic, M. Hoeger, A. Marn
Proc. ASME. GT2014, Volume 2C: Turbomachinery, V02CT38A053, June 16–20, 2014
Publisher: American Society of Mechanical Engineers
Paper No: GT2014-26915
https://doi.org/10.1115/GT2014-26915
View Paper titled, Comparison of the Experimental Results Between a 2D EGV Cascade Test and a Rig Test Under Engine Representative Conditions
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Topics: Cascades (Fluid dynamics), Engines, Aircraft engines, Bearings, Flow (Dynamics), Fluid mechanics, Guide vanes, Pressure, Stress, Thermoelectric coolers
Proceedings Papers

Influence of Endwall Contouring on the Transonic Flow in a Compressor Blade

M. Hoeger, P. Cardamone, L. Fottner
Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 759-768, June 3–6, 2002
Publisher: American Society of Mechanical Engineers
Paper No: GT2002-30440
https://doi.org/10.1115/GT2002-30440
View Paper titled, Influence of Endwall Contouring on the Transonic Flow in a Compressor Blade
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Topics: Blades, Compressors, Transonic flow, Flow (Dynamics), Shock (Mechanics), Mach number, Cascades (Fluid dynamics), Rotors, Shapes, Boundary layers
Proceedings Papers

Influencing the Secondary Losses in Compressor Cascades by a Leading Edge Bulb Modification at the Endwall

R. Mu¨ller, H. Sauer, K. Vogeler, M. Hoeger
Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 783-791, June 3–6, 2002
Publisher: American Society of Mechanical Engineers
Paper No: GT2002-30442
https://doi.org/10.1115/GT2002-30442
View Paper titled, Influencing the Secondary Losses in Compressor Cascades by a Leading Edge Bulb Modification at the Endwall
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Topics: Compressors, Vortices, Blades, Suction, Turbines, Boundary layers, Cascades (Fluid dynamics), Pressure measurement, Rotors, Wind tunnels
Journal Articles

Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage

M. Hoeger, G. Fritsch, D. Bauer
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 1999, 121(3): 456–468.
https://doi.org/10.1115/1.2841338
Published Online: July 1, 1999
View Article titled, Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage
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Topics: Computer simulation, Leakage, Shock (Mechanics), Vortices, Simulation, Flow (Dynamics), Blades, Compressors, Displacement, Instrumentation
Journal Articles

A Correlation for Tip Leakage Blockage in Compressor Blade Passages

M. Hoeger, M. Lahmer, M. Dupslaff, G. Fritsch
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2000, 122(3): 426–432.
https://doi.org/10.1115/1.1303707
Published Online: February 1, 1999
View Article titled, A Correlation for Tip Leakage Blockage in Compressor Blade Passages
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Topics: Blades, Compressors, Displacement, Flow (Dynamics), Leakage, Rotors, Mach number, Boundary layers, Simulation, Vortices