Department of Aeronautics and Astronautics: Recent submissions

Now showing items 64-66 of 503

    • Blade scale effects of tip leakage 

      Martinez-Sanchez, Manuel; Gauthier, R. P. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1990], 1990)
      The effects of blade-tip leakage in a turbine are investigated by modeling the stage as an incomplete actuator disk. It is found that the spanwise flow redistribution due to the gap is such as to produce a uniform unloading ...

    • Analysis and design of transonic cascades with splitter vanes 

      Youngren, H. H. (Harold Hayes) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1991, 1991)
      A new computational method, MISES, is developed for turbomachinery design and analysis applications. The method is based on the fully coupled viscous /inviscid method, ISES, and is applicable to blade-to-blade analysis of ...

    • A systematic study of supersonic jet noise 

      Louis, Jean F. (Jean François); Letty, Richard M.; Patel, Jayantilal R. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, 1971, 1971)
      The purpose of this work is to study the acoustic fields associated with two different nozzle configurations; a rectangular and a circular. Both nozzles are designed with the same exit Mach number and have an identical ...