Optimization and Computational Fluid Dynamics - Department of ...
Optimization and Computational Fluid Dynamics - Department of ...
Optimization and Computational Fluid Dynamics - Department of ...
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150 René A. Van den Braembussche<br />
attention in recent years. In what follows one will describe the fast, multipoint<br />
<strong>and</strong> multidisciplinary optimization method, developed at the von Kármán<br />
Institute, <strong>and</strong> its application to different turbomachinery designs.<br />
6.2 <strong>Optimization</strong> Methods<br />
<strong>Optimization</strong> methods attempt to determine the design variables Xi(i =1,n)<br />
that minimize an objective function OF(U(Xi),Xi)whereU(Xi)isthesolution<br />
<strong>of</strong> the flow equations R(U(Xi),Xi) = 0 <strong>and</strong> subject to nA performance<br />
constraints Aj(U(Xi),Xi) ≤ 0(j =1,nA) <strong>and</strong>nG geometrical constraints<br />
Gk(Xi) ≤ 0(k =1,nG).<br />
Specifying as Objective Function (OF) the difference between a prescribed<br />
<strong>and</strong> calculated pressure distribution results in an inverse design method. Aiming<br />
for the improvement <strong>of</strong> the overall performance leads to a global optimization<br />
technique.<br />
Numerical optimization procedures consist <strong>of</strong> the following components,<br />
described in more detail in the following paragraphs:<br />
• a choice <strong>of</strong> independent design parameters <strong>and</strong> the definition <strong>of</strong> the addressable<br />
part <strong>of</strong> the design space.<br />
• definition <strong>of</strong> an OF quantifying the performance. Any st<strong>and</strong>ard analysis<br />
tool can be used to calculate the components such as lift, drag, efficiency,<br />
mass flow, manufacturing cost or a combination <strong>of</strong> all <strong>of</strong> them.<br />
• a search mechanism to find the optimum combination <strong>of</strong> the design parameters,<br />
i.e., the one corresponding to the minimum <strong>of</strong> the OF.<br />
6.2.1 Search Mechanisms<br />
There are two main groups <strong>of</strong> search mechanisms:<br />
• Analytical ones calculate the required geometry changes in a deterministic<br />
way from the output <strong>of</strong> the performance evaluation. A common one is<br />
the steepest descent method approaching the area <strong>of</strong> minimum OF by<br />
following the path with the largest negative gradient on the OF surface<br />
(Fig. 6.2). This approach requires the calculation <strong>of</strong> the direction <strong>of</strong> the<br />
largest gradient <strong>of</strong> the OF <strong>and</strong> the step length. A comprehensive overview<br />
<strong>of</strong> gradient based optimization techniques is given by V<strong>and</strong>erplaats [17].<br />
• Zero-order or stochastic procedures require only function evaluations.<br />
They make a r<strong>and</strong>om or systematic sweep <strong>of</strong> the design space or use evolutionary<br />
theories such as Genetic Algorithms (GA) or Simulated Annealing<br />
(SA).