Gas Turbine Laboratory Reports: Recent submissions

Now showing items 121-123 of 123

    • Exit flow from a transonic compressor rotor 

      Thompkins, William T.; Kerrebrock, Jack L. (Cambridge : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1975], 1975)
      Summary: The three dimensional unsteady flow field behind a transonic compressor rotor with a design pressure ratio of 1.6 at a tip Mach number of 1.2 has been resolved on the blade-passing time scale, using the M.I.T. ...

    • Wake behavior downstream of a transonic compressor rotor 

      Stephens, Harry Elias (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1974, 1974)
      Measurements of the static pressure resolved in radial and axial directions downstream of a transonic compressor rotor have been harmonically analyzed. The investigation is part of a program addressing the behavior of ...

    • Attenuation of sound in lined circular ducts 

      Cho, Young-chung; Ingard, K. Uno (Cambridge : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1975], 1975)
      In the previous report, we have used approximate expressions for the wall impedance for the discussion of sound attenuation in lined circular ducts. For instance, Eq. (2.5) has been used for the wall impedance of a circular ...