An investigation of transition fixing technique for a 10.5% thick, 28 degrees sweptback wing at high subsonic speeds and R is semilar to 3 x 106
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An investigation of transition fixing technique for a 10.5% thick, 28 degrees sweptback wing at high subsonic speeds and R is semilar to 3 x 106
P. G. Hutton
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1228
Date:
1972
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Aeronautical Research Council Current Papers
[1393]
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