affiliation not provided to SSRN
Gas turbine, Biot number, Turbulence intensity, Wall thickness, Cross flow, Overall cooling effectiveness
Gas turbine, Leading edge, Crossflow intensity, Film cooling diameter, Attack angle
uncertainty quantification, aerothermal performance, Turbine blade, Multi-cavity Squealer Tip, sensitivity analysis
Gas turbine, Leading edge, Double swirl chamber, Film cooling, Crossflow intensity
Gas Turbine, Turbine Blade;Leading Edge, Double swirl cooling, Film Cooling
Gas turbine, Leading edge, Double swirl cooling, Large eddy simulation
Hydrogen-combustion turbines, Turbine endwall, Unsteady aerothermal performance, Flow pulsation patterns, Transient response characteristics