Browsing by Subject "Film Cooling Effectiveness"
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(2017-01-24)A detailed study of various geometric & flow parameters that influence the film cooling effectiveness of gas turbine blade leading edge region was carried out. The parameters studied include leading edge shape, effect of ...
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(2017-05-17)Turbine vanes are typically assembled as a section containing single or double airfoil units in an annular pattern. First stage guide vane assembly results in two common mating interfaces - a gap between combustor and vane ...