Cascade Tests of High Stagger Compressor Blades

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概要

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• The aim of this report is to obtain the two-dimensional performance of compressor cascade with high stagger. The results are as follows : 1) The test method to obtain two-dimensional performance of compressor cascades has been determined. 2) The tests were carried out successfully and the performances of compressor cascades were obtained for 31 combinations of the pitch chord ratio S/C=0.7,1.0,1.2,and the stagger angle ξ=45°, 50°, 60°, 65°to each of the camber C_<lo> =0.0,0.4,0.8,1.2. 3) The design points were selected and the design loading limits were derived from the cascade data.

• 一般社団法人日本機械学会の論文

著者

• Takahara Kitao

  Propulsion Division National Aeronautical Laboratory

• MATSUKI Masakatsu

  Propulsion Division, National Aeronautical Laboratory

• Matsuki Masakatsu

  Propulsion Division National Aeronautical Laboratory

• Matsuki M.

  Propulsion Division, National Aeronautical Laboratory

関連論文

• Cascade Tests of High Stagger Compressor Blades

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