Gas Turbine Laboratory: Recent submissions

Now showing items 55-57 of 123

    • Cascade performance with accelerated or decelerated axial velocity 

      Kubota, Shigeo (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959], 1959)
      A theoretical method to estimate the effect of axial velocity change through a cascade was investigated. The change of axial velocity was reproduced by distributing sinks and sources within the blade passages, and the ...

    • A cascade tunnel for investigation of rotating stall 

      Kriebel, Anthony R.; Stenning, Alan H. (Alan Hugh) (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1954], 1954)
      A test apparatus which will reproduce the rotating stall phenomenon found in axial compressors has been constructed and installed in the main wind tunnel circuit of the Gas Turbine Laboratory. The test section consists of ...

    • A study of the end wall boundary layer in an axial compressor blade row 

      Moore, Raymond W. (Raymond William); Richardson, David L. (Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1955], 1955)
      Turbulent end wall boundary layers in the hub region of axial compressor blade rows have been studied in the Gas Turbine Laboratory. Both analytical and experimental work are presented. An attempt was made to predict the ...