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Journal Articles

Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant

Shailendra Naik, Marc Henze, Manuel Wilhelm, Heinz-Peter Schiffer
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. February 2025, 147(2): 021013.
Paper No: TURBO-24-1243
https://doi.org/10.1115/1.4067237
Published Online: December 17, 2024
View Article titled, Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant
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Topics: Blades, Coolants, Cooling, Film cooling, Gas turbines, Temperature, Pressure, Power stations, Flow (Dynamics), Cavities
Proceedings Papers

Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant

Shailendra Naik, Marc Henze, Manuel Wilhelm, Heinz-Peter Schiffer
Proc. ASME. GT2024, Volume 7: Heat Transfer: Combustors; Heat Transfer: Film Cooling, V007T12A044, June 24–28, 2024
Publisher: American Society of Mechanical Engineers
Paper No: GT2024-128684
https://doi.org/10.1115/GT2024-128684
View Paper titled, Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant
Open the PDF for Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant in another window
Topics: Blades, Film cooling, Gas turbines, Power stations, Metals, Turbines, Airfoils, Coolants, Cooling, Pressure
Proceedings Papers

Heat Transfer Enhancement in a Double Sequential Impingement Channel

Michele Gaffuri, Peter Ott, Shailendra Naik, Marc Henze
Proc. ASME. GT2021, Volume 5B: Heat Transfer — General Interest; Internal Air Systems; Internal Cooling, V05BT15A007, June 7–11, 2021
Publisher: American Society of Mechanical Engineers
Paper No: GT2021-58913
https://doi.org/10.1115/GT2021-58913
View Paper titled, Heat Transfer Enhancement in a Double Sequential Impingement Channel
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Topics: Heat transfer, Pressure, Corners (Structural elements), Flow (Dynamics), Cooling, Heat transfer coefficients, Liquid crystals, Transients (Dynamics)
Proceedings Papers

Highly Accurate Delta Efficiency Measurements at the Large Scale Turbine Rig

Johannes Eitenmüller, Manuel Wilhelm, Leonhard Gresser, Tom Ostrowksi, Sebastian Leichtfuss, Heinz-Peter Schiffer, Christoph Lyko, Shailendra Naik
Proc. ASME. GT2019, Volume 2B: Turbomachinery, V02BT40A001, June 17–21, 2019
Publisher: American Society of Mechanical Engineers
Paper No: GT2019-90294
https://doi.org/10.1115/GT2019-90294
View Paper titled, Highly Accurate Delta Efficiency Measurements at the Large Scale Turbine Rig
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Topics: Turbines, Inflow, Clearances (Engineering), Design, Geometry, Accounting, Combustion chambers, High pressure (Physics), Nozzle guide vanes, Swirling flow
Journal Articles

Heat Transfer in an Oblique Jet Impingement Configuration With Varying Jet Geometries

Simon Schueren, Florian Hoefler, Jens von Wolfersdorf, Shailendra Naik
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. March 2013, 135(2): 021010.
Paper No: TURBO-11-1214
https://doi.org/10.1115/1.4006598
Published Online: November 1, 2012
View Article titled, Heat Transfer in an Oblique Jet Impingement Configuration With Varying Jet Geometries
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Topics: Flow (Dynamics), Heat transfer, Jets
Proceedings Papers

Heat Transfer in an Oblique Jet Impingement Configuration With Varying Jet Geometries

Simon Schueren, Florian Hoefler, Jens von Wolfersdorf, Shailendra Naik
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1067-1077, June 6–10, 2011
Publisher: American Society of Mechanical Engineers
Paper No: GT2011-45169
https://doi.org/10.1115/GT2011-45169
View Paper titled, Heat Transfer in an Oblique Jet Impingement Configuration With Varying Jet Geometries
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Topics: Heat transfer, Jets, Blades, Computer simulation, Cooling, Design, Displacement, Ducts, Flow (Dynamics), Gas turbines
Journal Articles

Heat Transfer Characteristics of an Oblique Jet Impingement Configuration in a Passage With Ribbed Surfaces

Florian Hoefler, Simon Schueren, Jens von Wolfersdorf, Shailendra Naik
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2012, 134(3): 031022.
https://doi.org/10.1115/1.4003084
Published Online: July 15, 2011
View Article titled, Heat Transfer Characteristics of an Oblique Jet Impingement Configuration in a Passage With Ribbed Surfaces
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Topics: Geometry, Heat transfer, Jets, Reynolds number, Transients (Dynamics), Flow (Dynamics)
Proceedings Papers

Heat Transfer Characteristics of an Oblique Jet Impingement Configuration in a Passage With Ribbed Surfaces

Florian Hoefler, Simon Schueren, Jens von Wolfersdorf, Shailendra Naik
Proc. ASME. GT2010, Volume 4: Heat Transfer, Parts A and B, 127-138, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-22288
https://doi.org/10.1115/GT2010-22288
View Paper titled, Heat Transfer Characteristics of an Oblique Jet Impingement Configuration in a Passage With Ribbed Surfaces
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Topics: Heat transfer, Jets, Reynolds number, Blades, Cooling, Flow (Dynamics), Gas turbines, Geometry, Heat capacity, Impingement cooling
Proceedings Papers

Heat Transfer in a Confined Oblique Jet Impingement Configuration

Florian Hoefler, Simon Schueren, Jens von Wolfersdorf, Shailendra Naik
Proc. ASME. GT2009, Volume 3: Heat Transfer, Parts A and B, 311-321, June 8–12, 2009
Publisher: American Society of Mechanical Engineers
Paper No: GT2009-59354
https://doi.org/10.1115/GT2009-59354
View Paper titled, Heat Transfer in a Confined Oblique Jet Impingement Configuration
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Topics: Heat transfer, Flow (Dynamics), Cooling, Impingement cooling, Jets, Reynolds number, Computer simulation, Discharge coefficient, Engineering simulation, Gas turbines
Proceedings Papers

Leading Edge Film Cooling and the Influence of Shaped Holes at Design and Off-Design Conditions

Guillaume Wagner, Peter Ott, Gregory Vogel, Shailendra Naik
Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 577-587, May 14–17, 2007
Publisher: American Society of Mechanical Engineers
Paper No: GT2007-27715
https://doi.org/10.1115/GT2007-27715
View Paper titled, Leading Edge Film Cooling and the Influence of Shaped Holes at Design and Off-Design Conditions
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Topics: Design, Film cooling, Pressure, Suction, Coolants, Cooling, Heat transfer, Jets, Liquid crystals, Momentum