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BAIL 2006 Book of Abstracts - Institut für Numerische und ...

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L. SAVIĆ, H. STEINRÜCK: Asymptotic Analysis <strong>of</strong> the mixed convection flow past a<br />

horizontal plate near the trailing edge<br />

✬<br />

✫<br />

<strong>of</strong> the plate ∆A interacts not only via the potential flow in the upper deck but also via the<br />

hydrostatic pressure in the main deck with the pressure ∆p in the lower deck. The interaction<br />

law for the pressure difference between the upper and lower side can be written in the form<br />

∆A ′ (x (3) ) + √ 3ash(x (3) �<br />

) x (3)� 1/3<br />

=<br />

� � 0 1 ∆ˆp(ξ) + 2as|ξ|<br />

−<br />

π −∞<br />

1/3<br />

x (3) dξ −<br />

− ξ<br />

1<br />

� ∞ As(ξ) − ash(ξ)|ξ|<br />

π −∞<br />

1/3<br />

x (3) �<br />

dξ<br />

− ξ<br />

Where As(x (3) ) is the displacement thickness obtained for the classical trailing edge problem<br />

[3, 1] and x (3) is the coordinate in the lower, main and upper deck parallel to the plate. Here as<br />

is a constant and h(.) the heayside function. It turns out that the difference pressure ∆p has a<br />

discontinuity at the trailing edge. Thus new sub-layers (in the main and lower deck) to resolve<br />

this discontinuity are introduced.<br />

In the following table we give an overview <strong>of</strong> the most important layers needed for the<br />

asymptotic analysis. We introduce the following notation according to the stretching factor as<br />

a power <strong>of</strong> the Reynolds number: x (α) = Re α/8 x and y (β) = Re β/8 y.<br />

α β flow region<br />

0 0 potential flow region<br />

0 4 bo<strong>und</strong>ary layer and wake<br />

3 3 upper deck<br />

3 4 main deck<br />

3 5 lower deck<br />

4 4 main deck - trailing edge<br />

5 5 lower deck - trailing edge<br />

Table 1: Scales <strong>of</strong> the different flow regions<br />

The new results <strong>of</strong> the analysis will be the local behavior <strong>of</strong> the difference pressure at the<br />

trailing edge. For both <strong>of</strong> the newly introduced sub-layers elliptic equations for the local pressure<br />

variation can be derived and will be solved numerically. Thus on triple deck scales there will be<br />

a flow aro<strong>und</strong> the trailing edge. Thus the perturbation <strong>of</strong> the classical triple deck problem by<br />

small buoyancy effects behaves quite differently than by small angles <strong>of</strong> attack [3].<br />

References<br />

[1] K. Stewartson, On the flow near the trailing edge <strong>of</strong> flat plate, Mathematika, 16, 106-121<br />

(1969).<br />

[2] A.F. Messiter, Bo<strong>und</strong>ary layer flow near the trailing edge <strong>of</strong> flat plate, SIAM J. Appl. Math.,<br />

18, 241-257, (1970).<br />

[3] R. Chow and R. E. Melnik, Numerical Solutions <strong>of</strong> Triple-Deck Equations for Laminar<br />

Trailing Edge Stall, Grumman Research Dept., Report RE-526J (1976).<br />

[4] W. Schneider and M. G. Wasel, Breakdown <strong>of</strong> the bo<strong>und</strong>ary-layer approximation for mixed<br />

convection flow above a horizontal plate, Int. J. Heat Transfer, 28, 2307-2313 (1985).<br />

[5] Lj. Savić and H. Steinrück, Mixed convection flow past a horizontal plate, Theoretical and<br />

Applied Mechanics, 32, 1-19 (2005).<br />

Speaker: STEINRÜCK, H. 42 <strong>BAIL</strong> <strong>2006</strong><br />

2<br />

✩<br />

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