Gas Turbine Laboratory: Recent submissions

Now showing items 97-99 of 123

    • The influence of tip clearance on stall limits of a rectilinear cascade of compressor blades 

      Khabbaz, Ghassan R. (Ghassan Raji) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959], 1959)
      An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a two dimensional rectilinear cascade. By using the mirror and image technique the end wall boundary layer ...

    • Asymmetric inlet flow in axial turbomachines 

      Seidel, Barry S. (Barry Stanley) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1959, 1959)
      A modified actuator disc analysis is made which, through an improved prediction of the blade forces, attempts to give closer correspondence with experiment than the previous theory. The fluid is assumed inviscid and ...

    • A secondary flow approach to the inlet vortex flow field 

      Viguier, Henri Charles (c1980, c1980)
      A theoretical study is presented of the fluid mechanics of the inlet vortex (or ground vortex). The vorticity field associated with this phenomenon is investigated using a secondary flow approach. In this approach the flow ...