Department of Aeronautics and Astronautics: Recent submissions

Now showing items 61-63 of 503

    • UNSFLO : a numerical method for the calculation of unsteady flow in turbomachinery 

      Giles, M. (Michael) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1991], 1991)
      Introduction: There are four principal sources of unsteadiness in a single stage of a turbomachine in which there is one row of stationary blades (stators) and one row of moving blades (rotors). As shown in Fig. 1.1, ...

    • 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 ...

    • 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 ...