UNCERTAINTY QUANTIFICATION OF NON-DIMENSIONAL PARAMETERS FOR A FILM COOLING CONFIGURATION IN SUPERSONIC CONDITIONS

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 it is highly probable that shock impingement will occur in proximity to a row of cooling holes.The presence of such a shoc

read more



CFD Analysis of Passive Autocatalytic Recombiner

In water-cooled nuclear power reactors, significant quantities of hydrogen could be produced following a postulated loss-of-coolant accident (LOCA) along with nonavailability of emergency core cooling system (ECCS).Passive autocatalytic recombiners (PAR) are implemented in the containment of water-cooled power reactors to mitigate the risk of hydro

read more