GT2021-58457 In-Stall Compressor Performance and the Effects of Reynolds Number

von Hutchings, Jack
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2021)

GT2020-15384 The Effects of Reynolds Number on the Stall and Pre-Stall Behaviour of Compact Axial Compressors

von Hutchings, Jack
Veröffentlicht in ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 2, A (2020)

GT2022-82177 Effects of Sideslip Direction on a Rear Fuselage Boundary Layer Ingesting Fan

von Pardo, Alejandro Castillo
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2022)

Fluid mechanics and thermodynamics of turbomachinery

von Dixon, Sydney L.
Veröffentlicht 2014

FLOW FIELD AND POWER BALANCE OF A DISTRIBUTED AFT-FUSELAGE BOUNDARY LAYER INGESTING AIRCRAFT

von Tse, Tze Sing
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Inlets, nozzles and propulsion systems integration (2020)

Fluid mechanics and thermodynamics of turbomachinery

von Dixon, Sydney Lawrence
Veröffentlicht 2014

GT2020-16296 Fan Aerodynamics With a Short Intake at High Angle of Attack

von Mohankumar, Ben
Veröffentlicht in ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 2, A (2020)

GT2021-58569 Sweep Effects on Fan-Intake Aerodynamics at High Angle of Attack

von Mohankumar, Ben
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2021)

GT2021-59851 An Experimental Investigation Into the Impacts of Varying the Circumferential Extent of Tip-Low Total Pressure Distortion on Fan Stability

von Allen, Oliver
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2021)

GT2022-82039 Fan Stability Enhancement With Partial Casing Treatments

von Oldfield, Matthew K.
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2022)

Fluid mechanics and thermodynamics of turbomachinery

von Dixon, Sydney L.
Veröffentlicht 2010

GT2021-59284 Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade

von Liu, Qiang
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics (2021)

Aerodynamic design and performance of an over-wing low pressure ratio fan stage

von Giesecke, Daniel
Veröffentlicht 2022