A Cascade Investigation of a Convection- and Film-cooled Turbine Vane Made from Radially Stacked Laminates |
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A Cascade Investigation of a Convection- and Film-cooled Turbine Vane Made ... Herbert J. Gladden No preview available - 1974 |
Common terms and phrases
0.76 millimeter airfoil boundary layer Comparison of laminated cooled vane Cooling air corrected Cross-sectional schematic data presented data reported diffusion bonding discussed in reference edge suction surface equation excess material experimental data fabrication film FILM-COOLED TURBINE VANE fin effectiveness flow channels four vanes full-coverage film-cooled vane gas and coolant gas temperature gas-flow ratio gas-side surface impingement kg/sec laminated convection laminated sheet-type material laminated vane Leading edge suction Lewis Research Center M-Tc metering pores midchord midspan N/cm² newtons per square ŋATR Perforated insert 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 distribution temperature of 920 test vanes Thermocouple location Total inlet gas trailing edge region Trailing edge suction transpiration cooled transpiration-cooled vane unpublished data vane row vane surface vane tested wall temperature wire cloth vane