RADICAL SOLUTIONS FOR EDUCATION IN AFRICA: OPEN EDUCATION AND SELF-DIRECTED LEARNING IN THE CONTINENT.



Uncertainty Quantification of Non-Dimensional Parameters for a Film Cooling Configuration in Supersonic Conditions

In transonic high-pressure turbine stages, oblique shocks originating from vane trailing edges impact the suction side of each adjacent vane.High-pressure vanes are cooled to tolerate the combustor exit-temperature levels, then Waterproof Ponchos it is highly probable that shock impingement will occur in proximity to a row of cooling holes.The pres

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