High reynolds number tests on an unswept 11% thick RAE 101 section aerofoil
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High reynolds number tests on an unswept 11% thick RAE 101 section aerofoil
R. W. F. Gould
;
C. F. Cowdrey
;
P. G. G. O'Neill
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/544
Date:
1961
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Aeronautical Research Council Current Papers
[1393]
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