GT2022-81623 Approximating Gas Turbine Combustor Exit Temperature Distribution Factors Using Spatially Under-Sampled Measurements

von Lou, Fangyuan
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, B: Turbomachinery: Axial flow turbine aerodynamics; deposition, erosion, fouling, and icing; radial turbomachinery aerodynamics (2022)

GT2022-81623 Approximating Gas Turbine Combustor Exit Temperature Distribution Factors Using Spatially Under-Sampled Measurements

von Lou, Fangyuan
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, B: Turbomachinery: Axial flow turbine aerodynamics; deposition, erosion, fouling, and icing; radial turbomachinery aerodynamics (2022)

GT2020-14867 Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data: Part 1 -- Methodology and Sensitivity Analysis

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

GT2020-14247 Compressor Stall Warning Using Nonlinear Feature Extraction Algorithms

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

GT2021-59210 In Choosing the Optimal Impeller Exit Velocity Triangles in Preliminary Design

von Lou, Fangyuan
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, C: Turbomachinery: Design methods and CFD modeling for turbomachinery; ducts, noise, and component interactions (2021)

CONCEPTUAL DESIGN OF A 10-PASSENGER THIN-HAUL ELECTRIC AIRCRAFT

von Yang, Boning
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Electric aircraft technologies (2020)

GT2021-60103 Details of Shrouded Stator Hub Cavity Flow in a Multi-Stage Axial Compressor Part 1: Interactions Nith the Primary Flow

von Kamdar, Nitya
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)

GT2021-60115 Jetails of Shrouded Stator Hub Cavity Flow in a Multi-Stage Axial Compressor Part 2: Leakage Flow Characteristics in Stator Wells

von Kamdar, Nitya
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)

GT2022-83509 Reconstructing Turbine Non-Uniform Flow Including Hot Streaks Using Spatially Under-Sampled Measurements

von Zhu, Xu
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, B: Turbomachinery: Axial flow turbine aerodynamics; deposition, erosion, fouling, and icing; radial turbomachinery aerodynamics (2022)

INVESTIGATION OF SLIP MODELS FOR HIGH-SPEED CENTRIFUGAL COMPRESSORS

von Harrison, Herbert M.
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Gas turbine engines ; Volume 1 of 2 (2019)

GT2022-83509 Reconstructing Turbine Non-Uniform Flow Including Hot Streaks Using Spatially Under-Sampled Measurements

von Zhu, Xu
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, B: Turbomachinery: Axial flow turbine aerodynamics; deposition, erosion, fouling, and icing; radial turbomachinery aerodynamics (2022)

GT2022-82682 Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part 1 — Surge Signature

von Lou, Fangyuan
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, D: Turbomachinery: Multidisciplinary design approaches, optimization, and uncertainty quantification; turbomachinery general interest; unsteady flows in turbomachinery (2022)

GT2022-82686 Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part 2 — Correlation With Subecomponent Characteristics

von Lou, Fangyuan
Veröffentlicht in ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, D: Turbomachinery: Multidisciplinary design approaches, optimization, and uncertainty quantification; turbomachinery general interest; unsteady flows in turbomachinery (2022)

GT2021-59968 Accounting for Circumferential Flow Nonuniformity in a Multi-Stage Axial Compressor

von Lou, Fangyuan
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)

GT2020-15465 Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data: Part 2 -- Practical Application for Experiments

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