Concepedia

The effect of effusion holes inclination angle on the adiabatic film cooling effectiveness in a three-sector gas turbine combustor rig with a realistic swirling flow

Antonio Andreini, Riccardo Becchi, Bruno Facchini, Alessio Picchi, Antonio Peschiulli

International Journal of Thermal Sciences · 2017 · 63 citations · 38 references

Open access

Concepts

EngineeringMechanical EngineeringPhysicsCombustionFluid DynamicsHeat TransferCombustion FundamentalsCombustion ProcessesCombustion ThermodynamicsGas Turbine CombustionGas Turbine EnginesCombustor AerodynamicsCombustor DesignCombustor DynamicsCombustor GeometryTurbine AerodynamicsTurbine Blade AerodynamicsTurbine Blade CoolingTurbine Cooling

References

38

Describing Uncertainty in Single Sample Experiments

S. J. Kline · Mechanical Engineering · 1953 · 6.6K citations

Computing, Mathematics, Statistics +11

Fundamentals of digital particle image velocimetry

Jerry Westerweel · Measurement Science and Technology · 1997 · 1.4K citations

Engineering, Computer Science, Diagnostic Imaging +8

Power generation and aeropropulsion gas turbines: From combustion science to combustion technology

S.M. Correa · Symposium (International) on Combustion · 1998 · 189 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

GASEOUS FILM COOLING WITH MULTIPLE INJECTION STATIONS

J. P. Sellers · AIAA Journal · 1963 · 164 citations

Engineering, Mechanical Engineering, Heat Transfer +5

Film cooling characteristics of a single round hole at various streamwise angles in a crossflow: Part I effectiveness

C.H.N. Yuen, R.F. Martinez-Botas · International Journal of Heat and Mass Transfer · 2002 · 164 citations

Engineering, Mechanical Engineering, Fluid Dynamics +10