Gas Turbine Laboratory: Recent submissions

Now showing items 58-60 of 123

    • Boundary layer on an airfoil in a cascade 

      Peterson, Carl R. ([Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1958], 1958)
      A study of the turbulent boundary layer on an airfoil in a cascade is presented. The major portion of the observations are on the suction surface of the airfoil. The effect of added diffusion across the cascade due to a ...

    • Stall propagation in axial compressors 

      Stenning, Alan H. (Alan Hugh) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1955], 1955)
      A theory of stall propagation in a cascade of airfoils of high solidity has been developed which includes the effects of finite blade chord and of the boundary layer response to changes in angle of attack. The theory is ...

    • Temperature wake in an adverse pressure gradient 

      Sturek, Walter B. (Walter Beynon) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1961], 1961)
      A study is made of the flow pattern resulting from the presence of a temperature wake in a uniform velocity field subjected to various adverse pressure gradients. Dimensionless temperature profiles and velocity profiles ...