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 ... Method of brazing an article and assembly for brazing a stator ...Turbine Thermal Barrier Coatings,? H.E. Eaton; N.S. Bornstein; J.T.. DeMarcin. ASME 96-GT-283. ?Capacitive Measurement Of Compressor And Turbine Blade Tip To.
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