PIV investigation of the flow characteristics in internal coolant passages of gas turbine airfoils with two ducts connected by a sharp 180° bend

Keywords: Turbomachinery ; Heat Transfer ; Measurement Techniques These Ecole polytechnique federale de Lausanne EPFL, n° 1816 (1998)Laboratoire de thermique appliquee et de turbomachines Reference doi:10.5075/epfl-thesis-1816Print copy in library catalog Record created on 2007-04-25, modified on 2016-08-08