Tag Archives: EXPERIMENTAL TECHNIQUE

Facility for Investigating the Flow in a Low Pressure Turbine Exit Structure

Design and Operation of a Low Speed Test Turbine Facility

Influence of a Multi-Hole Pressure Probe on the Flow Field in Axial-Turbines

Entropy Wave Generator for Indirect Combustion Noise Experiments in a High-Pressure Turbine

Aircraft engine sensor fault detection, isolaton and reconfiguration using fuzzy logic control based unknown input observer

Model-based control and diagnostic techniques for operational improvements of gas turbine engines

Predicted performance of brush seals: Porous medium versus resolved bristle matrix and comparison with experimental data