Now showing items 1-2 of 2

    • Flutter and forced response of mistuned rotors using standing wave analysis 

      Bundas, David J.; Dugundji, John (Cambridge, Mass. : Gas Turbine & Plasma Dynamics Laboraotry, [1983], 1983)
      The torsion flutter and forced response of tuned and mistuned cascades is examined using a standing wave approach, as opposed to the traditional traveling wave approach used in cascades aerodynamic models. The motion of ...
    • 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 ...