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Proceedings Papers

Estimation of Resultant Airframe Forces for a Variable Pitch Fan Operating in Reverse Thrust Mode

David John Rajendran, Richard Tunstall, Vassilios Pachidis

Proc. ASME. GT2022, Volume 1: Aircraft Engine; Ceramics and Ceramic Composites, V001T01A024, June 13–17, 2022

Paper No: GT2022-82446

DOI: https://doi.org/10.1115/GT2022-82446

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Topics: Flow (Dynamics), Thrust

Journal Articles

Estimation of Resultant Airframe Forces for a Variable Pitch Fan Operating in Reverse Thrust Mode

David John Rajendran, Richard Tunstall, Vassilios Pachidis

J. Eng. Gas Turbines Power. December 2022, 144(12): 121017.

Paper No: GTP-22-1306

DOI: https://doi.org/10.1115/1.4055489

Published Online: October 14, 2022

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Topics: Aircraft, Engines, Flow (Dynamics), Thrust, Drag (Fluid dynamics)

Journal Articles

On the Use of an Inflatable Rubber Lip to Improve the Reverse Thrust Flow Field in a Variable Pitch Fan

David John Rajendran, Vassilios Pachidis

J. Eng. Gas Turbines Power. November 2021, 143(11): 111019.

Paper No: GTP-21-1290

DOI: https://doi.org/10.1115/1.4051961

Published Online: October 5, 2021

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Topics: Design, Engines, Flow (Dynamics), Rubber, Thrust, Aircraft, Nozzles

Proceedings Papers

On the Use of an Inflatable Rubber Lip to Improve the Reverse Thrust Flow Field in a Variable Pitch Fan

David John Rajendran, Vassilios Pachidis

Proc. ASME. GT2021, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture, V001T01A015, June 7–11, 2021

Paper No: GT2021-59526

DOI: https://doi.org/10.1115/GT2021-59526

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Topics: Flow (Dynamics), Rubber, Separation (Technology), Thrust

Journal Articles

Flow Distortion Into the Core Engine for an Installed Variable Pitch Fan in Reverse Thrust Mode

David John Rajendran, Vassilios Pachidis

J. Turbomach. July 2021, 143(7): 071001.

Paper No: TURBO-20-1252

DOI: https://doi.org/10.1115/1.4050331

Published Online: April 8, 2021

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Topics: Engines, Flow (Dynamics), Pressure, Thrust, Separation (Technology)

Proceedings Papers

Flow Distortion Into the Core Engine for an Installed Variable Pitch Fan in Reverse Thrust Mode

David John Rajendran, Vassilios Pachidis

Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A005, September 21–25, 2020

Paper No: GT2020-14174

DOI: https://doi.org/10.1115/GT2020-14174

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Topics: Engines, Flow (Dynamics), Thrust

Proceedings Papers

Fan Flow Field in an Installed Variable Pitch Fan Operating in Reverse Thrust for a Range of Aircraft Landing Speeds

David John Rajendran, Vassilios Pachidis

Proc. ASME. GT2019, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards, V001T01A017, June 17–21, 2019

Paper No: GT2019-91039

DOI: https://doi.org/10.1115/GT2019-91039

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Topics: Aircraft, Flow (Dynamics), Thrust, Engines, Nozzles, Air flow, Design, Ducts, Exhaust systems, Guide vanes

Journal Articles

Fan Flow Field in an Installed Variable Pitch Fan Operating in Reverse Thrust for a Range of Aircraft Landing Speeds

David John Rajendran, Vassilios Pachidis

J. Eng. Gas Turbines Power. October 2019, 141(10): 101018.

Paper No: GTP-19-1333

DOI: https://doi.org/10.1115/1.4044686

Published Online: September 20, 2019

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Topics: Flow (Dynamics), Engines, Thrust, Aircraft

Proceedings Papers

Design and Analysis of Radial Turbine for Turbocharger Application

Bharathan Raghavan Desikan, David John Rajendran, Sharad Kapil, Seepana Venkata Ramana Murty, Deshkulkarni Kishore Prasad

Proc. ASME. GTINDIA2017, Volume 1: Compressors, Fans and Pumps; Turbines; Heat Transfer; Combustion, Fuels and Emissions, V001T02A011, December 7–8, 2017

Paper No: GTINDIA2017-4860

DOI: https://doi.org/10.1115/GTINDIA2017-4860

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Topics: Design, Turbines, Turbochargers, Wheels, Compressors, Computer software, Exhaust systems, Gases, Internal combustion engines, Kinetic energy

Proceedings Papers

Aerodynamic Performance of an Unlocated High Pressure Turbine Rotor With Worn Tip Seal Fins

Lucas Pawsey, David John Rajendran, Vassilios Pachidis

Proc. ASME. GT2017, Volume 2A: Turbomachinery, V02AT40A023, June 26–30, 2017

Paper No: GT2017-64312

DOI: https://doi.org/10.1115/GT2017-64312

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Topics: Fins, High pressure (Physics), Rotors, Turbines, Displacement, Manufacturing, Blades, Failure, Geometry, Stators