Gas Turbine Laboratory: Recent submissions

Now showing items 34-36 of 123

    • A coupled Euler/Navier-Stokes algorithm for 2-D unsteady transonic shock/boundary-layer interaction 

      Allmaras, Steven R. (Steven Richard) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1989], 1989)
      This thesis presents a coupled Euler/Navier-Stokes algorithm for solving 2-D unsteady transonic flows. The flowfield is described by a Defect formulation, where separate Euler and Navier-Stokes algorithms are used on ...

    • Effects of compressor endwall suction and blowing on stability enhancement 

      Lee, Norman Kai Wing (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1988], 1988)
      An experimental investigation was carried out to examine the effects on stall margin of flow injection into, and removal out of, the endwall region of an axial compressor blade row. A main goal was to identify the mechanism ...

    • UNSFLO : a numerical method for unsteady inviscid flow in turbomachinery 

      Giles, M. (Michael) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1988, 1988)
      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, ...