Browsing Gas Turbine Laboratory Reports by Subject "Aerofoils"

Now showing items 1-3 of 3

    • Cascade performance with accelerated or decelerated axial velocity 

      Kubota, Shigeo (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959], 1959)
      A theoretical method to estimate the effect of axial velocity change through a cascade was investigated. The change of axial velocity was reproduced by distributing sinks and sources within the blade passages, and the ...

    • Newton solution of steady two-dimensional transonic flow 

      Giles, M. (Michael) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985], 1985)
      A new method is developed for the solution of the steady, two-dimensional Euler equations for transonic flows. The discrete steady-state equations are derived in conservative finite-volume form on an intrinsic streamline ...

    • Thin airfoils in rotational flow 

      Kotansky, Donald Richard (Cambridge, Mass : Massachusetts Institute of Technology, [1965], 1965)
      The problem of rotational or shear flow about thin airfoils has been investigated theoretically and experimentally. The theoretical approach is based on the concept of a lifting line in a bounded shear flow whose primary ...