Curves suitable for families of aerofoils with variable maximum thickness position, nose radius, camber and nose droop
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Curves suitable for families of aerofoils with variable maximum thickness position, nose radius, camber and nose droop
L. H. tanner
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/371
Date:
1957
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Aeronautical Research Council Current Papers
[1393]
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