Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) June 13-17, 2022, Rotterdam, The Netherlands Volume 6 Heat transfer A Combustors, film cooling

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Körperschaften: ASME Turbo Expo (VerfasserIn), International Gas Turbine Institute (SponsorIn)
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Sprache:eng
Veröffentlicht: New York, N.Y. the American Society of Mechanical Engineers 2022
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Titel Jahr Verfasser
GT2022-81345 Assessment of a Conjugate Heat Transfer Method on an Effusion Cooled Combustor Operated With a Swirl Stabilized Partially Premixed Flame 2022 Amerini, A.
GT2022-82128 Numerical Prediction of Heat Transfer Coefficient and Adiabatic Effectiveness on a Nozzle Guide Vane With Representative Combustor Outflow 2022 Tomasello, Stella Grazia
GT2022-83803 Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics 2022 Petit, Sylvain
GT2022-79528 Identification of Fluctuation Modes for a Cylindrical Film Cooling Hole Using the Spectral Proper Orthogonal Decomposition Method 2022 Rosafio, Nicola
GT2022-78519 Optimized Film Cooling Flow on a Contoured Endwall Within a Transonic Annular Cascade 2022 Burdett, Timothy A.
GT2022-7 9023 Large Eddy Simulation Based Optimization of a Fan-Shaped Cooling Hole Geometry to Enhance Cooling Performance 2022 Agarwal, Shubham
GT2022-80810 Conjugate Heat Transfer of Cylindrical and Trenched Film Cooling Designs With Array Jet Impingement 2022 Fischer, Lukas
GT2022-81161 Heat Transfer Coefficient and Adiabatic Effectiveness on a Film-Cooled Pressure Side: Results and Assessment of the IR-Based Measurement Technique Reliability 2022 Bacci, T.
GT2022-81520 The Effect of Diffuser Shape for Film Cooling Holes With Constant Expansion Angles and Area Ratio 2022 Lundburg, Evan
GT2022-81826 Scaling Flat Plate Overall Effectiveness Measurements 2022 McNamara, Luke J.
GT2022-81923 Effects of Freestream Turbulence on Air-Mist Film Cooling: Two-Phase Flow Simulations 2022 Dwivedi, Anjali
GT2022-02189 Effect of Location and Rotational Reynolds Number on Film Cooling of Rotating Blade Pressure Side 2022 Long, Meng
GT2022-82203 Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor- Turbine Interface Geometry Part 2: Describing the Coolant Coverage 2022 Nawathe, Kedar P.
GT2022-82514 Effects of Internal Coolant Crossflow on Film-Cooling Performance of Double-Jet and Cylindrical Holes 2022 Zhu, Huaitao
GT2022-82726 Evaluation of Adjoint Optimized Hole - Part Il: Parameter Effects on Performance 2022 Yoon, Christopher
GT2022-83169 Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High- Speed Relative Casing Motion 2022 Xie, Wenbo
GT2022-82139 Numerical Study of Combustor-Turbine Interaction by Using Hybrid RANS-LES Approach 2022 Tomasello, Stella Grazia
GT2022-82697 Turbine Vane Passage Experiments Documenting Evolution of Secondary Flows Witr Changes in Combustor Coolant Injection Flowrates 2022 Nawathe, Kedar P.
GT2022-82178 Experimental Investigation of Effusion Film Cooling on a Cylindrical Leading Edge Model 2022 Huang, I-Cheng
GT2022-82118 Experimental Investigation of the Effects of Thermal Barrier Coating on Twisted Blade Full Film Cooling 2022 Yan, Hao-nan
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