Gas Turbine Laboratory: Recent submissions

Now showing items 28-30 of 123

    • Blade scale effects of tip leakage 

      Martinez-Sanchez, Manuel; Gauthier, R. P. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1990], 1990)
      The effects of blade-tip leakage in a turbine are investigated by modeling the stage as an incomplete actuator disk. It is found that the spanwise flow redistribution due to the gap is such as to produce a uniform unloading ...

    • A systematic study of supersonic jet noise 

      Louis, Jean F. (Jean François); Letty, Richard M.; Patel, Jayantilal R. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1971, 1971)
      The purpose of this work is to study the acoustic fields associated with two different nozzle configurations; a rectangular and a circular. Both nozzles are designed with the same exit Mach number and have an identical ...

    • Separation of turbulent, incompressible flow from a curved, backward-facing step 

      Nice, George Roland; Tseng, W.-Y. (Wu-Yang); Moses, Hal Lynwood (Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine Laboratory, [1966], 1966)
      An experimental investigation of turbulent, incompressible flow separation over curved and sharp, backward-facing steps is presented with results for various step heights. Mean velocities in the separating boundary layer ...