GT2021-59384 Reduced-Order Models for Effusion Modelling in Gas Turbine Combustors

GT2021-59384 Reduced-Order Models for Effusion Modelling in Gas Turbine Combustors

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Bibliographische Detailangaben
Veröffentlicht in:ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 5, A: Heat transfer: Combustors, film cooling
1. Verfasser: Paccati, S. (VerfasserIn)
Weitere Verfasser: Mazzei, L. (VerfasserIn), Andreini, A. (VerfasserIn), Facchini, B. (VerfasserIn)
Pages:2021
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
Schlagworte:
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Titel Jahr Verfasser
GT2021-59217 Analysis of Swirl Number Effects on Effusion Flow Behaviour Using Time Resolved PIV 2021 Lenzi, T.
GT2021-59384 Reduced-Order Models for Effusion Modelling in Gas Turbine Combustors 2021 Paccati, S.
GT2021-59429 Influence of Opposing Dilution Jets on Effusion Cooling 2021 Creer, M. Riley
GT2021-59687 High-Resolution Thermal Profiling of a Combustor in a Non-Dedicated Test Using Thermal History Coatings 2021 Peral, David
GT2021-59015 Improving the Film Cooling Performance of a Turbine Endwall With Multi-Fidelity Modeling Considering Conjugate Heat Transfer 2021 Bu, Hongyan
GT2021-59150 DDES Numerical Investigations on Coherent Structures in Trailing-Edge Film Cooling Combined With Pressure-Side Film Hole 2021 Xiao, Xiangtao
GT2021-59496 The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames 2021 Jagerhofer, Patrick R.
GT2021-59312 Effect of Spanwise Hole to Hole Spacing on Overall Cooling Effectiveness of Effusion Cooled Combustor Liners for a Swirl Stabilized Can Combustor 2021 Ahmed, Shoaib
GT2021-58451 Film Cooling Effectiveness Enhancement Using Multi-Longitudinal Vortex Generated by Alternating Elliptical Film Holes 2021 Xiao, Kun
GT2021-58661 Analysis of LES and 1D Hot-Wire Data to Determine Actively Generated Main Flow Turbulence in a Film Cooling Test Rig 2021 Fischer, Lukas
GT2021-59269 Uncertainty Analysis of Film Cooling of Fan-Shaped Holes on a Stator Vane Under Realistic Inlet Conditions 2021 Wang, Hai
GT2021-59332 Adjoint Optimization of Film Cooling Hole Geometry 2021 Jones, Fraser B.
GT2021-59602 Effect of a Ceramic Matrix Composite Surface on Film Cooling 2021 Wilkins, Peter H.
GT2021-59663 Effect of Self-Sustained Pulsation of Coolant Flow on Adiabatic Effectiveness and Net Heat Flux Reduction on a Flat Plate 2021 Rosafio, Nicola
GT2021-59825 Coupling of Mainstream Velocity Fluctuations With Plenum Fed Film Cooling Jets 2021 Sperling, Spencer
GT2021-58889 Unsteady Film Cooling Performance on the High Pressure Turbine Shroud Under Rotor-Stator Interaction for an Aero-Engine 2021 Bao, Zihao
GT2021-59196 Autonomous Large Eddy Simulations Setup for Cooling Hole Shape Optimization 2021 Agarwal, Shubham
GT2021-59366 Influence of Coolant Density on Turbine Blade Film Cooling at Transonic Cascade Flow Conditions Using the Pressure Sensitive Paint Technique 2021 Ullah, Izhar
GT2021-59638 Fow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes 2021 Cubeda, S.
GT2021-59780 CFD Evaluation of Internal Flow Effects on Turbine Blade Leading-Edge Film Cooling With Shaped Hole Geometries 2021 Easterby, Christopher C.
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