Browsing Gas Turbine Laboratory Reports by Subject "Blades"

Now showing items 1-3 of 3

    • Prediction of three-dimensional compressible turbulent boundary layers on transonic compressor blades 

      Usab, William J., Jr. (William James) (c1980, c1980)
      A small crossflow approximation to the full three dimensional compressible turbulent boundary layer equations for turbomachine blade rows is developed by taking advantage of the nature of blade geometry and inviscid flow ...

    • Role of flow alignment and inlet blockage on vaned diffuser performance 

      Phillips, Michael Stephen (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1997, 1997)
      A computational investigation of the effects of inlet conditions on straight-channel diffuser performance is undertaken. The steady, three-dimensional, Navier-Stokes solver used for the investigation is found to adequately ...

    • A study of outlet guide vanes 

      Qvale, Einar Björn (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1963], 1963)
      A criterion for design of unstalled compressor blades has been proposed, and a set of outlet guide vanes has been designed according to this criterion and has been tested. A typical compressor stator and outlet guide vane ...