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Numerical Study on the Effect of Rim Seal Slot Filleting on Turbine Endwall Cooling Performance

https://doi.org/10.2139/ssrn.4641840
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inferredcites →https://doi.org/10.1016/j.applthermaleng.2006.10.017openalex-extracted
Numerical heat transfer predictions and mass/heat transfer measurements in a linear turbine cascade
inferredcites →https://doi.org/10.1016/j.applthermaleng.2015.11.103openalex-extracted
DES study of blade trailing edge cutback cooling performance with various lip thicknesses
inferredcites →https://doi.org/10.1016/j.applthermaleng.2016.08.172openalex-extracted
Effect of purge flow on endwall flow and heat transfer characteristics of a gas turbine blade
inferredcites →https://doi.org/10.1016/j.applthermaleng.2018.05.088openalex-extracted
Effects of location and profile of upstream slot on the endwall aerothermal performance of a gas turbine blade
inferredcites →https://doi.org/10.1016/j.expthermflusci.2011.11.010openalex-extracted
Disk cavity purge air outflow into the main gas path of a model turbine stage
inferredcites →https://doi.org/10.1016/j.expthermflusci.2019.109888openalex-extracted
Measurements of detailed heat transfer characteristics on a high-pressure turbine vane endwall with coolant injection
inferredcites →https://doi.org/10.1016/j.ijheatfluidflow.2013.08.012openalex-extracted
Purge flow and interface gap geometry influence on the aero-thermal performance of a rotor blade cascade
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2016.02.014openalex-extracted
Numerical study on the effects of slot injection configuration and endwall alignment mode on the film cooling performance of vane endwall
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2017.08.072openalex-extracted
Effects of upstream slot geometry on the endwall aerothermal performance of a gas turbine blade under different ejection angle conditions
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2018.11.153openalex-extracted
Effect of gas turbine endwall misalignment with slashface leakage on the blade endwall aerothermal performance
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2020.120565openalex-extracted
Film Cooling Patterns over an Aircraft Engine Turbine Endwall with Slot Leakage and Discrete Hole Injection
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2021.121034openalex-extracted
Effect of misalignment at 2nd vane endwall on heat transfer with purge flow
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2021.121626openalex-extracted
Aero-thermal optimization of a gas turbine blade endwall with non-axisymmetric contouring and purge flow
inferredcites →https://doi.org/10.1016/j.jppr.2012.10.007openalex-extracted
An experimental investigation on the trailing edge cooling of turbine blades
inferredcites →https://doi.org/10.1115/1.1312807openalex-extracted
High Free-Steam Turbulence Effects on Endwall Heat Transfer for a Gas Turbine Stator Vane
inferredcites →https://doi.org/10.1115/1.1397308openalex-extracted
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness
inferredcites →https://doi.org/10.1115/1.1400113openalex-extracted
Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint
inferredcites →https://doi.org/10.1115/1.1811099openalex-extracted
Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First-Stage Vane
inferredcites →https://doi.org/10.1115/1.2720484openalex-extracted
Experimental Investigation of Turbine Leakage Flows on the Three-Dimensional Flow Field and Endwall Heat Transfer
inferredcites →https://doi.org/10.1115/1.2812950openalex-extracted
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
inferredcites →https://doi.org/10.1115/1.2841006openalex-extracted
Flow Visualization in a Linear Turbine Cascade of High Performance Turbine Blades
inferredcites →https://doi.org/10.1115/1.3230352openalex-extracted
Crossflows in a Turbine Cascade Passage
inferredcites →https://doi.org/10.1115/1.4000578openalex-extracted
Influence of Rim Seal Purge Flow on the Performance of an Endwall-Profiled Axial Turbine
inferredcites →https://doi.org/10.1115/1.4002950openalex-extracted
The Effect of the Combustor-Turbine Slot and Midpassage Gap on Vane Endwall Heat Transfer
inferredcites →https://doi.org/10.1115/1.4002964openalex-extracted
Trailing Edge Film Cooling of Gas Turbine Airfoils—External Cooling Performance of Various Internal Pin Fin Configurations
inferredcites →https://doi.org/10.1115/1.4003838openalex-extracted
The Effect of Coolant Injection on the Endwall Flow of a High Pressure Turbine
inferredcites →https://doi.org/10.1115/1.4028432openalex-extracted
Experimental Investigation of Purge Flow Effects on a High Pressure Turbine Stage
inferredcites →https://doi.org/10.1115/2001-gt-0146openalex-extracted
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II — Heat Transfer and Film-Cooling Effectiveness
inferredcites →https://doi.org/10.1115/95-gt-001openalex-extracted
Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using the Ammonia and Diazo Technique
inferredcites →https://doi.org/10.1115/gt2007-27867openalex-extracted
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
inferredcites →https://doi.org/10.1115/gt2010-23578openalex-extracted
Trailing Edge Film Cooling of Gas Turbine Airfoils: External Cooling Performance of Various Internal Pin Fin Configurations
inferredcites →https://doi.org/10.1115/imece2009-12847openalex-extracted
The Effect of the Combustor-Turbine Slot and Mid-Passage Gap on Vane Endwall Heat Transfer
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