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    • 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 ...