An Experimental Test Case for Transonic Low-Pressure Turbines – Part I: Rig Design, Instrumentation and Experimental Methodology

Autor: Simonassi, Loris, Lopes, Gustavo, Gendebien, Samuel, Torre, Antonino Federico Maria, Patinios, Marios, Lavagnoli, Sergio, Zeller, Nicolas, Pintat, Ludovic

Publikováno v: Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics

The ultra-high bypass ratio geared turbofan is a key concept to reduce the environmental impact of the next generation aircrafts. The increase in rotational speed of the low-pressure turbine (LPT) enabled by the geared architecture offers potential b

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https://zenodo.org/record/8174514