A technique of design analysis for the gas turbine engine regenerator with complanar channels according to the heat flow and hydraulic resistance
V. A. Trushin,A. Yu. ChechulinVolume:
57
Language:
english
Journal:
Russian Aeronautics (Iz VUZ)
DOI:
10.3103/S1068799814010139
Date:
January, 2014
File:
PDF, 331 KB
english, 2014