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Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford

A. C. Browning et al.
Aerade · Other
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aeronauticsaerospaceaviationengineering
aerospace, aeronautics, engineering, aviation
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