Now showing items 55-57 of 503

    • Feedback stabilization of compression systems 

      Simon, Jonathan S. (Jonathan Seth) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993, 1993)
      An experimental and analytical study was conducted on the use of feedback stabilization to extend the stable operating range of compression and pumping systems. Prevention of surge, in aircraft gas turbine engines, an ...
    • Computational simulation of unsteady flow in transonic compressor rotor 

      Owen, Philip Ray (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1986], 1986)
      The unsteady flow about a section of a modern first stage transonic compressor rotor was simulated using a finite difference approximation to the two-dimensional, Reynolds averaged, unsteady, compressible, viscous Navier-Stokes ...
    • Aerodynamics of aircraft engines : stride and stumbles 

      Cumpsty, N. A. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992, 1992)
      Summary: Attempts to understand and predict the aerodynamic behaviour of compressors and turbines in aircraft gas turbines have been encouraged by the intense competitive pressure which exists. Many of the apparently most ...