GT2020-16183 Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 2, D
1. Verfasser: Tao, Zhi (VerfasserIn)
Weitere Verfasser: Guo, Zhendong (VerfasserIn), Song, Liming (VerfasserIn), Li, Jun (VerfasserIn)
Pages:2020
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2020
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
GT2020-14180 Numerical Study on Duct Acoustic Modal and Source Flow Structure of Fan Tones With Leaned and Swept Stator 2020 Liangfeng, Wang
GT2020-14233 Noise Attenuation Potential Using Helmholtz Absorbers Integrated in Low Pressure Turbine Exit Guide Vanes and Turbine Exit Casing End Walls 2020 Zenz, Manuel
GT2020-14798 Impact of Turbine-Strut Clocking on the Performance of a Turbine Center Frame 2020 Sterzinger, P. Z.
GT2020-14927 Super Aggressive S-Ducts for Air Breathing Rocket Engines 2020 Taylor, J. V.
GT2020-15299 Experimental Investigation of Gas Turbine Axial Diffuser Performance: Part I -- Parametric Analysis of Influential Variables 2020 Brown, Kenneth
GT2020-16318 An Experimental, Aerodynamic Evaluation of Design Choices for a Low-Pressure Compressor Transition Duct 2020 Walker, A. Duncan
GT2020-14139 Usage of Data Provenance Models in Collaborative Multi-Disciplinary Aero-Engine Design 2020 Reitenbach, S.
GT2020-14382 Prediction of Non-Linear Mechanical Behavior With Deep Neural Network: Application on Low Pressure Turbine Disc 2020 Jin, Yuan
GT2020-14668 Introduction of a Novel Parameter Model to Analyze the Geometric Variation of Airfoil Edges of Ex-In-Service Compressor Airfoils 2020 Voigt, Paul
GT2020-14580 Multidisciplinary Design Optimization of a Low-Noise and Efficient Next-Generation Aero-Engine Fan 2020 Jaron, Robert
GT2020-14900 Optimization of the Workflow of Multistage Axial Compressors Using Modern Gas Dynamics Computing Systems 2020 Popov, Grigorii
GT2020-15166 Uncertainty Based Optimization Strategy for the Gappy-POD Multi-Fidelity Method 2020 Poethke, Bernhard
GT2020-15218 Sensitivity Analysis and Uncertainty Quantification for Rim Seal Ingestion With 1-D Network Models 2020 Dominguez, Alejandro Pozo
GT2020-15207 Industrial Challenges in Large Thermally Enabled Structural Whole Engine Models 2020 Tindall, Michelle
GT2020-15847 Multidisciplinary Design of a Low-Noise Propeller: Part II -- Efficient Aero-Acoustic- Mechanical Design Methodology Exploiting Surrogate Models in an Adaptive Design Space 2020 Baert, Lieven
GT2020-16183 Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation 2020 Tao, Zhi
GT2020-14166 Investigation of the Loss Generation in a Turning Vane Frame at Different Inlet Turbulence Conditions 2020 Riebl, Sebastian F.
GT2020-14161 Measurements of Multiple Pure Tone Propagation From a High Bypass Turbofan Rotor in an Internal Flow Facility 2020 Bozak, Richard F.
GT2020-14444 Control of the Aero-Engine Nacelle Intake Flow Separation Caused by Crosswind Condition Using Plasma Actuation 2020 Zhang, Haideng
GT2020-14897 Numerical Investigation of the Low Pressure Compressor Tone Noise of a High Bypass Ratio Turofan 2020 Rossikhin, Anton
Alle Artikel auflisten