Gas Turbine Laboratory: Recent submissions

Now showing items 49-51 of 123

    • An investigation of rotating stall in a single stage axial compressor 

      Montgomery, Stephen Ross; Braun, Joseph J. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1955], 1955)
      The rotating stall characteristics of a single stage axial flow compressor were investigated. The number of stall cells and their propagation velocities were found with and without stator blades. The measured velocities ...

    • FORTRAN program for calculating three-dimensional, inviscid, rotational flows with shock waves in axial compressor blade rows : I--user's manual 

      Thompkins, William T. (Cambridge, Mass. : Gas Turbine & Plasma Dynamics Laboratory, Massachusetts Institute of Technology, [1981], 1981)
      Summary: A FORTRAN-IV computer program has been developed for the calculation of the inviscid transonic/supersonic flow field in a fully three-dimensional blade passage of an axial compressor rotor or stator. Rotors may ...

    • 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 ...