28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
THE EXPERIENCE OF HIGH PRESSURE RATIO SINGLE STAGE HPT DESIGNING
V. D. Venediktov, V. G Krupa, S. V. Rudenko, A. D. Nepomnyashchiy, V. K. Sichev*, A. A. Shvirev*
CIAM, Moscow, Russia; *"Aviadvigatel", Russia
Keywords: experimental module, high-pressure turbine, intermediate duct
Some results of calculated and experimental investigations of the high loading single-stage cooled high-pressure turbine (HPT) for a turbofan engine of the civil aviation are shown in this paper.
view full paper