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D. K. Hall
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Journal Articles

Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes

D. K. Hall, E. M. Greitzer, C. S. Tan
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2023, 145(3): 031008.
Paper No: TURBO-22-1226
https://doi.org/10.1115/1.4055645
Published Online: October 17, 2022
View Article titled, Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes
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Topics: Design, Flow (Dynamics), Pressure, Rotors, Stators, Guide vanes
Journal Articles

Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

D. K. Hall, E. M. Greitzer, A. Uranga, M. Drela, S. A. Pandya
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2022, 144(10): 101002.
Paper No: TURBO-21-1308
https://doi.org/10.1115/1.4054035
Published Online: April 7, 2022
View Article titled, Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation
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Topics: Aircraft, Boundary layers, Flow (Dynamics), Pressure, Computation, Engines
Proceedings Papers

Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

D. K. Hall, E. M. Greitzer, A. Uranga, M. Drela, S. A. Pandya
Proc. ASME. GT2021, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture, V001T01A010, June 7–11, 2021
Publisher: American Society of Mechanical Engineers
Paper No: GT2021-59079
https://doi.org/10.1115/GT2021-59079
View Paper titled, Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation
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Topics: Boundary layers, Engines, Flow (Dynamics), Aircraft, Computation, NASA, Pressure, Bubbles, Fans, Inflow
Journal Articles

Fan Performance Scaling With Inlet Distortions

J. J. Defoe, M. Etemadi, D. K. Hall
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. July 2018, 140(7): 071009.
Paper No: TURBO-18-1016
https://doi.org/10.1115/1.4039433
Published Online: June 22, 2018
View Article titled, Fan Performance Scaling With Inlet Distortions
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Topics: Diffusion (Physics), Flow (Dynamics), Pressure, Rotors, Stators, Enthalpy, Temperature
Journal Articles

Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion

D. K. Hall, E. M. Greitzer, C. S. Tan
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research-Article
J. Turbomach. July 2017, 139(7): 071012.
Paper No: TURBO-16-1310
https://doi.org/10.1115/1.4035631
Published Online: March 7, 2017
View Article titled, Analysis of Fan Stage Conceptual Design Attributes for Boundary Layer Ingestion
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Topics: Blades, Design, Flow (Dynamics), Rotors, Stators, Pressure, Enthalpy, Diffusion (Physics), Geometry
Proceedings Papers

Fan Performance Scaling With Inlet Distortions

J. J. Defoe, D. K. Hall
Proc. ASME. GT2016, Volume 2A: Turbomachinery, V02AT37A052, June 13–17, 2016
Publisher: American Society of Mechanical Engineers
Paper No: GT2016-58009
https://doi.org/10.1115/GT2016-58009
View Paper titled, Fan Performance Scaling With Inlet Distortions
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Topics: Blades, Compressors, Computer simulation, Design, Diffusion (Physics), Engines, Fans, Flow (Dynamics), Geometry, Inflow
Proceedings Papers

Analysis of Fan Stage Design Attributes for Boundary Layer Ingestion

D. K. Hall, E. M. Greitzer, C. S. Tan
Proc. ASME. GT2016, Volume 2A: Turbomachinery, V02AT37A047, June 13–17, 2016
Publisher: American Society of Mechanical Engineers
Paper No: GT2016-57808
https://doi.org/10.1115/GT2016-57808
View Paper titled, Analysis of Fan Stage Design Attributes for Boundary Layer Ingestion
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Topics: Boundary layers, Design, Flow (Dynamics), Rotors, Stators, Blades, Turbomachinery, Energy resources, Geometry, Momentum
Proceedings Papers

Performance Limits of Axial Compressor Stages

D. K. Hall, E. M. Greitzer, C. S. Tan
Proc. ASME. GT2012, Volume 8: Turbomachinery, Parts A, B, and C, 479-489, June 11–15, 2012
Publisher: American Society of Mechanical Engineers
Paper No: GT2012-69709
https://doi.org/10.1115/GT2012-69709
View Paper titled, Performance Limits of Axial Compressor Stages
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Topics: Compressors, Cycles, Design, Boundary layer turbulence, Gas turbines, Machinery, Thermal efficiency