1.

Select the flow which is not laminar all over the thin airfoil at =0 .
The given values are for Rec.

A. 7 10<sup>5</sup>
B. 9 10<sup>4</sup>
C. 2 10<sup>3</sup>
D. We can t say with just this information
Answer» B. 9 10<sup>4</sup>


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