GT2021-58798 Performance Evaluation of Leading Edge Tubercles Applied to the Blades in a 2-D Compressor Cascade

von Sidhu, Satpreet S.
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)

Effect of Leading Edge Tubercles on Tilt-Wing Transition

von Sim, Felix
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Aircraft design ; Volume 1 of 2 (2022)

GT2021-58849 Internal Aerodynamic Performance Evaluation of Double Entrance S-Duct Intake at Moderately Aigh Subsonic Mach Number

von Sidhu, Satpreet
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 1: Aircraft engine, fans and blowers, marine, wind energy, scholar lecture (2021)

Effect of a Passive Flow Control Device on the Performance of an S-Duct Inlet in High Subsonic Flow

von Rider, Courtney
Veröffentlicht in ASME Turbo Expo (2023 : Boston, Mass.) Proceedings of ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition (GT 2023) ; Volume 1: Aircraft engine (2023)

GT2021-60230 Investigation of a Passive Flow Control Device in an S-Duct Inlet at High Subsonic Flow

von Rider, Courtney
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 1: Aircraft engine, fans and blowers, marine, wind energy, scholar lecture (2021)

Effect of Entrance Cross-Section on Bulk Swirl and Performance of an S-Duct Inlet in High Subsonic Flow

von Gilbart, Ben
Veröffentlicht in ASME Turbo Expo (2023 : Boston, Mass.) Proceedings of ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition (GT 2023) ; Volume 1: Aircraft engine (2023)