Tests in the compressed air tunnel on two aerofoil sections having a large scale effect on CLmax at a critical reynolds number
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Tests in the compressed air tunnel on two aerofoil sections having a large scale effect on CLmax at a critical reynolds number
C. Salter
;
H. M. Lee
;
R. C. Owen
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/105
Date:
1952
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Aeronautical Research Council Current Papers
[1393]
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