Browsing Gas Turbine Laboratory Reports by Subject "Aerodynamic load"

Now showing items 1-4 of 4

    • Boundary layer effects on airfoil lift 

      Schneider, Kurt H. (Kurt Herbert) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958], 1958)
      A study of the discrepancy in lift between potential flow calculations and experiments was made. In potential flow the fluid is assumed to follow the contour of the airfoil, forming a stagnation point at the geometric ...

    • Comparative study of tip clearance effects in compressors and turbines 

      Yokoyama, Eiji (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1961], 1961)
      The influence of tip clearance on the lift distribution along a blade span was studied on linear compressor and turbine cascades. The wall boundary layer was removed by means of the image technique. The lift distribution ...

    • 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 ...

    • Stall propagation in a cascade of airfoils 

      Kriebel, Anthony R. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1956], 1956)
      An experimental investigation of stall propagation in a stationary circular cascade by means of high speed schlieren and interferometer photography is described. This investigation suggests an analytical approach to the ...