1. 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): doi: /
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.