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 Photo Paper occur in proximity to a row of cooling holes.The presence of

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Use of content management systems to address nursing workflow

Nurses are at the forefront of providing healthcare services to individuals of all age groups and with varying medical conditions.Aside from the critical knowledge and technical skills from nursing science, advancement in technology has assisted nurses in delivering quality nursing care by streamlining workflow processes and ensuring that data can

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