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Optimization and Computational Fluid Dynamics - Department of ...

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118 Nicolas R. Gauger<br />

CL := 1<br />

�<br />

Cp(ny cosα − nx sinα)dl ,<br />

Cref C<br />

Cm :=<br />

(5.6)<br />

1<br />

C2 �<br />

Cp(ny(x − xm) − nx(y − ym)) dl .<br />

ref C<br />

(5.7)<br />

If the geometry is now perturbed from C(X) toC(X + δX), then via the<br />

solution <strong>of</strong><br />

where<br />

∂(w + δw)<br />

∂t<br />

⇔ ∂(δw)<br />

∂t<br />

+ ∂(f + δf)<br />

∂x<br />

+ ∂(δf)<br />

∂x<br />

+ ∂(g + δg)<br />

+ ∂(δg)<br />

∂y<br />

∂y<br />

=0<br />

=0 inD (5.8)<br />

n ⊤ v =0 on C = C(X + δX) , (5.9)<br />

the associated variation <strong>of</strong> pressure is as follows<br />

Finally via<br />

<strong>and</strong><br />

δCp = 2δp<br />

γM2 ∞p∞ 2(p(X + δX) − p(X))<br />

≈<br />

γM2 ∞p∞ . (5.10)<br />

δnx ≈ nx(X + δX) − nx(X) (5.11)<br />

δny ≈ ny(X + δX) − ny(X) (5.12)<br />

the variations <strong>of</strong> CD, CL <strong>and</strong> Cm are obtained as<br />

2<br />

δCD =<br />

γM2 �<br />

δp(nx cosα + ny sinα) dl<br />

∞p∞Cref C<br />

+ 1<br />

�<br />

Cp(δnx cosα + δny sinα) dl , (5.13)<br />

Cref<br />

δCL =<br />

2<br />

C<br />

γM 2 ∞ p∞Cref<br />

+ 1<br />

Cref<br />

�<br />

C<br />

�<br />

C<br />

δp(ny cosα − nx sinα) dl<br />

Cp(δny cosα − δnx sinα) dl , (5.14)<br />

2<br />

δCm =<br />

γM2 ∞p∞C2 �<br />

δp(ny(x − xm) − nx(y − ym)) dl<br />

ref C<br />

�<br />

Cpδ(ny(x − xm) − nx(y − ym)) dl . (5.15)<br />

+ 1<br />

C 2 ref<br />

C<br />

Proceeding as described above for the n perturbations δiX in each <strong>of</strong> the n<br />

components <strong>of</strong> the design vector X, the gradient <strong>of</strong> the cost function I (e.g.,

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