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45 psia 76 millimeter airfoil boundary layer Comparison of laminated convection-cooled cooled vane cooling air corrected Cross-sectional schematic data presented data reported data were taken diffusion bonding discussed in reference edge suction surface equation excess material experimental data fabrication figure 3(a film FILM-COOLED TURBINE VANE fin effectiveness four vanes full-coverage film-cooled vane gas and coolant gas-flow ratio gas-side surface impingement kg/sec laminated convection laminated sheet-type material laminated vane Leading edge suction Lewis Research Center metering pores Midchord midspan N/cm newtons per square Performing Organization plenum pore-plenum-slot combination pressure of 1640 pressure surface reference 7 vane region of vane shown in figure slave vanes stagnation point suction surface region temperature and pressure temperature of 920 test points test vanes Thermocouple location Total coolant flow Total inlet gas trailing edge region Trailing edge suction transpiration cooled transpiration-cooled vane unpublished data vane row vane surface vane tested wall temperature wire cloth vane