Gas Turbine Laboratory: Recent submissions

Now showing items 55-57 of 123

    • Boundary layer separation ; preliminary report 

      Moses, Hal Lynwood (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1962], 1962)
      The phenomenon of incompressible boundary layer separation and the existing methods of predicting it are discussed. The failure of these theories in many cases clearly indicates a need for further investigation. A program ...

    • A study of the end wall boundary layer in an axial compressor blade row 

      Moore, Raymond W. (Raymond William); Richardson, David L. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1955], 1955)
      Turbulent end wall boundary layers in the hub region of axial compressor blade rows have been studied in the Gas Turbine Laboratory. Both analytical and experimental work are presented. An attempt was made to predict the ...

    • 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 ...