By Barus C.
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Additional info for An Adjustment in Relation to the Fresnel Coefficient(en)(6s)
This means that in the disturbed flow region the total variation of the displacement thickness is δ∗ ∼ δ∗(3) . From the physical standpoint this can be easily understood if it is recalled that for p 1 only slow near-wall streamtubes can vary strongly in thickness. 4) dp ε2 ∼ 3 dx λ It remains to note that these estimates no longer hold for λ ≤ ε, since in this case the condition p 1 is violated. Flows with p ∼ 1 are considered in Chapter 3. Moreover, we will not consider flows in which the pressure gradient induced upon interaction is smaller in the order than that on the main part of the body surface, where it is of the order O(1).
Further, it is invalid. For a semi-infinite separation zone the solution must be also considered for x ≥ O(1). At distances x ∼ 1 the thickness of the mixing zone 6, in which the leading viscous and inertial terms of the Navier-Stokes equations are of the same order, is equal to O(ε). The distance from the ψ = 0 line to the body is of the order ε1/2 . Thus, a region O must exist, in which the flow is inviscid in the first approximation. In fact, on the scale of region O, region 6 is simply a line into which the gas with v ∼ ε is sucked.
In Figs. 6 we have plotted parameter profiles across region 3 (see Fig. 2) of the boundary layer. In the main part of the layer the profiles of the velocity and other parameters are of little interest, since in region 2 with thickness of the order of ε any variations are small. It can be seen that the return flow velocities are relatively low. 8 0 1 2 3 4 5 η Fig. 5. , following from the similarity law) it should be remembered that they were obtained in the first approximation and their relative error is O(Re−1/8 ).
An Adjustment in Relation to the Fresnel Coefficient(en)(6s) by Barus C.