High-temperature high-frequency turbine exit flow field measurements in a military engine with a cooled unsteady total pressure probe
Proceedings of the Institution of Mechanical Engineers / A ; 225 , 7 ; 954-964
2011
Article (Journal)
English
BKL: | 52.50 Energietechnik: Allgemeines / 52.30 Strömungskraftmaschinen, Turbomaschinen / 52.30 / 52.50 | |
Local classification TIB: | 275/5345/5365/5500 |
Steady-unsteady measurements of the flow field downstream of a transonic high-pressure turbine stage
Online Contents | 2001
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