On the theory of laminar boundary layers involving separation (1934)
NASA Technical Reports Server (NTRS) · leaf 14
ue of <ps is obtained from the separation criterion as the basic velocity used in defining the Eeynolds U Number of the problem, then we may take U (trailing edge) = l in accordance with (3). Once again to fix ideas we may consider our airfoil only in the normal range of angles of attack, so that… … 0 <Pi <P Figure 0—The single-roof potential velocity profile as the limiting case of a double- .20 roof profile. to trailing edge as the characteristic length of the problem, the dimensionless coordinate x along the surface will have values between zero at the stagnation .10 point and unity at the…
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