Wind tunnel tests between M = 0.4 and 2.0 on a cambered wing of slender ogee planform
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Wind tunnel tests between M = 0.4 and 2.0 on a cambered wing of slender ogee planform
M. D. Dobson
;
R. King-Underwood
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/791
Date:
1965
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Aeronautical Research Council Current Papers
[1393]
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