Now showing items 82-84 of 123

    • The development of a perturbed, incompressible, turbulent boundary layer 

      Handa, Hisayuki (Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1969], 1969)
      The response of a fully-developed equilibrium turbulent boundary layer to a small disturbance was observed experimentally under low-Mach number conditions: a turbulent boundary layer in an axisymmetric channel under zero ...
    • Condensation of supersaturated organic vapors in a supersonic nozzle 

      Dawson, Daniel Bogert (Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1967], 1967)
      Experiments were performed involving condensation of supersaturated benzene and chloroform vapors in a supersonic nozzle, with compressed air as the carrier gas. Experiments showed that the magnitude of the water vapor ...
    • Wall-shear-stress and laminarisation in accelerated turbulent compressible boundary-layers 

      Nash-Weber, James Ludlow (Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine Laboratory, [1968], 1968)
      Turbulent-laminar transition in compressible, steeply-accelerated, adiabatic, turbulent boundary layers on a smooth wall was investigated experimentally in the ranges of Mach and Reynold's numbers typical of nozzles used ...