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EXPERIMENTAL FLOW CONDITIONS
EXPERIMENTAL RESULTS WITHOUT EJECTION
3 other sections not shown
accelerated adiabatic wall effectiveness adiabatic wall temperature air film boundary layer displacement boundary layer thickness coolant cooling with ejection copper elements corresponding curves curvilinear coordinate dp/dx Effect of main EFFECTIVENESS FOR FLAT ejected flow ejected mass flow ejection angle ejection elements ejection hole diameter experimental feed tubes film cooling effectiveness flat plate ejection flow boundary layer flow Mach number further downstream gas turbine blades Goldstein heat transfer coefficient influence injection inlet investigations jets laminar boundary layer laminar nose layer displacement thickness leading edge main flow boundary main flow Mach main flow velocity main stream Mass Transfer mass velocity ratio Metzger model nose obtained perspex ratio G reduced Nusselt number row of ejection Seban secondary flow shown in Fig stagnation point ejection stagnation pressure stagnation temperature streamwise vortices surface test plate test section thermal conductivity thermocouples thickness to ejection turbulent boundary layer turbulent nose upstream velocity profiles x/d FIG