A non-axisymmetric end-wall boundary-layer theory for axial compressor rows
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A non-axisymmetric end-wall boundary-layer theory for axial compressor rows
J.W. Railly
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1335
Date:
1975
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Aeronautical Research Council Current Papers
[1393]
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