Nondestructive Testing Structural Health Monitoring of Gas Turbine ...
... stator around the tips of the rotor blades. All calculated K values are considered to be the approximate machine constants of eachrotor-stator configuration.
Design Solutions for Reducing Losses in Aeronautical Low ... - FLOREMeasurements were made on and around the outlet stator row of a 1.5-stage axial compressor using thermal anemometry. Pitch-wise hot-wire probe traverses were ... The development of a water dynamometer for turbine test applications.Summary.--The Reynolds-number effects on the performance of a single-stage compressor have been measured over the range 0.08 × 105 to 9.0 × 105. Unsteady boundary layer transition on axial compressor bladesthe opening is a feather seal slot in a stator for a gas turbine engine, the stator having a wall extending over the slot which is thinner ...
Autres Cours:
