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Keyword [High pressure gas turbine]
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1. Coherent anti-Stokes Raman scattering for quantitative temperature and concentration measurements in a high-pressure gas turbine combustor rig
2. Influence of rotor blade scaling on the numerical simulation of a high pressure gas turbine
3. Experimental Investigation of the Effect of Engine Representative Combustor Exit Temperature Profile and Disc Cavity Leakage Flow on the Film Cooling of Contoured Hub Endwall of a High Pressure Gas Turbine Rotor Cascade
4. Development of the control and ignition systems on a high pressure gas turbine combustor
5. The aerodynamic effects of wheelspace coolant injection into the mainstream flow of a high pressure gas turbine
6. Experimental Cascade Simulation of First Stage High Pressure Gas Turbine with Effects of Leakage Flow and Contouring on Endwall Film Cooling
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