Design Solutions for Reducing Losses in Aeronautical Low ... - FLORE
Measurements 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 ... The Effect of Reynolds Number on the Performance of a Single ...(a) Area-averaged pressure over the R1 blade surface (b) Relationship between pressure and tip leakage flow over blade tip ... chord length of the blade ... turbine ...
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