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Proceedings Papers

Measurements of the Convection Heat Transfer Coefficient for a Two-Dimensional Wall Jet: Uniform Temperature and Uniform Heat Flux Boundary Conditions

R. S. AbdulNour, K. Willenborg, J. J. McGrath, J. F. Foss, B. S. AbdulNour

Proc. ASME. IMECE97, Heat Transfer: Volume 3, 109-116, November 16–21, 1997

Publisher: American Society of Mechanical Engineers

Paper No: IMECE1997-0899

https://doi.org/10.1115/IMECE1997-0899

View Paper titled, Measurements of the Convection Heat Transfer Coefficient for a Two-Dimensional Wall Jet: Uniform Temperature and Uniform Heat Flux Boundary Conditions

Topics: Boundary-value problems, Convection, Heat flux, Temperature, Heat transfer coefficients, Infrared imaging, Thermal boundary layers, Thermocouples, Turbulence, Wall temperature

Proceedings Papers

Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

K. Willenborg, V. Schramm, S. Kim, S. Wittig

Proc. ASME. GT2000, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A091, May 8–11, 2000

Publisher: American Society of Mechanical Engineers

Paper No: 2000-GT-0290

https://doi.org/10.1115/2000-GT-0290

View Paper titled, Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

Topics: Heat transfer, Honeycomb structures, Heat transfer coefficients, Stators, Flow (Dynamics), Geometry, Engines, Finite element analysis, Jet engines, Pressure

Proceedings Papers

Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

V. Schramm, K. Willenborg, S. Kim, S. Wittig

Proc. ASME. GT2000, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A092, May 8–11, 2000

Publisher: American Society of Mechanical Engineers

Paper No: 2000-GT-0291

https://doi.org/10.1115/2000-GT-0291

View Paper titled, Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

Topics: Flow (Dynamics), Honeycomb structures, Geometry, Stators, Aircraft engines, Turbulence

Proceedings Papers

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

K. Willenborg, S. Kim, S. Wittig

Proc. ASME. GT2001, Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration, V003T01A010, June 4–7, 2001

Publisher: American Society of Mechanical Engineers

Paper No: 2001-GT-0123

https://doi.org/10.1115/2001-GT-0123

View Paper titled, Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

Topics: Heat transfer, Leakage, Pressure, Reynolds number, Heat transfer coefficients, Sealing (Process), Clearances (Engineering), Compressibility, Discharge coefficient, Finite element analysis

Proceedings Papers

3D-LDA Measurements in an Aero-Engine Bearing Chamber

Ph. Gorse, K. Willenborg, S. Busam, J. Ebner, K. Dullenkopf, S. Wittig

Proc. ASME. GT2003, Volume 5: Turbo Expo 2003, Parts A and B, 257-265, June 16–19, 2003

Publisher: American Society of Mechanical Engineers

Paper No: GT2003-38376

https://doi.org/10.1115/GT2003-38376

View Paper titled, 3D-LDA Measurements in an Aero-Engine Bearing Chamber

Topics: Aircraft engines, Bearings, Flow (Dynamics), Air flow, Drops, Industrial lubrication systems, Laser Doppler anemometry, Lubrication, Pressure, Reliability

Proceedings Papers

Experimental Studies of the Boundary Conditions Leading to Oil Fire in the Bearing Chamber and in the Secondary Air System of Aeroengines

K. Willenborg, S. Busam, H. Roßkamp, S. Wittig

Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 739-747, June 3–6, 2002

Publisher: American Society of Mechanical Engineers

Paper No: GT2002-30241

https://doi.org/10.1115/GT2002-30241

View Paper titled, Experimental Studies of the Boundary Conditions Leading to Oil Fire in the Bearing Chamber and in the Secondary Air System of Aeroengines

Topics: Bearings, Boundary-value problems, Fire, Ignition, Design, Engines, Lubricants, Pipes, Vents, Firing

Proceedings Papers

Experimental Analysis of Air/Oil Separator Performance

K. Willenborg, M. Klingsporn, S. Tebby, T. Ratcliffe, P. Gorse, K. Dullenkopf, S. Wittig

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 1495-1505, May 8–11, 2006

Publisher: American Society of Mechanical Engineers

Paper No: GT2006-90708

https://doi.org/10.1115/GT2006-90708

View Paper titled, Experimental Analysis of Air/Oil Separator Performance

Topics: Air flow, Aircraft engines, Bearings, Design, Diffraction, Drops, Engines, Experimental analysis, Flow (Dynamics), Lasers

Journal Articles

Experimental Analysis of Air∕Oil Separator Performance

K. Willenborg, M. Klingsporn, S. Tebby, T. Ratcliffe, P. Gorse, K. Dullenkopf, S. Wittig

Publisher: ASME

J. Eng. Gas Turbines Power. November 2008, 130(6): 062503.

https://doi.org/10.1115/1.2795785

Published Online: August 28, 2008

View Article titled, Experimental Analysis of Air∕Oil Separator Performance

Topics: Air flow, Drops, Flow (Dynamics), Separation (Technology), Pressure drop

Journal Articles

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

K. Willenborg, S. Kim, S. Wittig

Publisher: ASME

J. Turbomach. October 2001, 123(4): 815–822.

https://doi.org/10.1115/1.1397304

Published Online: February 1, 2001

View Article titled, Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

Topics: Discharge coefficient, Heat transfer, Leakage, Pressure, Reynolds number, Flow (Dynamics), Geometry, Stators

Journal Articles

Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

K. Willenborg, V. Schramm, S. Kim, S. Wittig

Publisher: ASME

J. Eng. Gas Turbines Power. January 2002, 124(1): 133–139.

https://doi.org/10.1115/1.1403459

Published Online: February 1, 2000

View Article titled, Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

Topics: Flow (Dynamics), Heat transfer, Heat transfer coefficients, Honeycomb structures, Rotors, Stators, Pressure, Temperature, Geometry

Journal Articles

Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

V. Schramm, K. Willenborg, S. Kim, S. Wittig

Publisher: ASME

J. Eng. Gas Turbines Power. January 2002, 124(1): 140–146.

https://doi.org/10.1115/1.1403460

Published Online: February 1, 2000

View Article titled, Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

Topics: Flow (Dynamics), Honeycomb structures, Leakage, Discharge coefficient

Journal citation

NARROW

Measurements of the Convection Heat Transfer Coefficient for a Two-Dimensional Wall Jet: Uniform Temperature and Uniform Heat Flux Boundary Conditions

Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

3D-LDA Measurements in an Aero-Engine Bearing Chamber

Experimental Studies of the Boundary Conditions Leading to Oil Fire in the Bearing Chamber and in the Secondary Air System of Aeroengines

Experimental Analysis of Air/Oil Separator Performance

Experimental Analysis of Air∕Oil Separator Performance

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

Influence of a Honeycomb Facing on the Heat Transfer in a Stepped Labyrinth Seal

Influence of a Honeycomb Facing on the Flow Through a Stepped Labyrinth Seal

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