Department of Aeronautics and Astronautics: Recent submissions

Now showing items 40-42 of 503

    • Parametric dependencies of aeroengine flutter for flutter clearance applications 

      Khalak, Asif, 1972- (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [2000], 2000)
      This thesis describes the effects of operational parameters upon aeroengine flutter stability. The study is composed of three parts: theoretical development of relevant parameters, exploration of a computational model, and ...

    • Measurements of rotor stalling in a matched and a mismatched multistage compressor 

      Silkowski, Peter D. (Peter Daniel) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1995], 1995)
      This paper presents the results from a set of experiments on stall inception in multistage axial flow compressors. The experiments were tailored to investigate phenomena having a wide range of time and length scales. This ...

    • A computational model for rotating stall and inlet distortions in multistage compressors 

      Gong, Yifang, 1964- (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1999], 1999)
      This thesis presents the conceptualization and development of a computational model for describing three-dimensional non-linear disturbances associated with instability and inlet distortion in multistage compressors. ...