Date of download: 10/14/2017 Copyright © ASME. All rights reserved. From: Experimental and Computational Study of the Effect of Momentum-Flux Ratio on High-Pressure Nozzle Guide Vane Endwall Cooling Systems J. Turbomach. 2017;139(12):121002-121002-14. doi:10.1115/1.4037756 Figure Legend: Computer-aided design model and components of the super-scale platform cooling facility: (a) front view and (b) rear view. A—vane and platforms, B—rear cameras, C—front cameras, D—combustor simulator, E—tailboards, F—hub cassette, and G—casing cassette.