Design optimization methods for rectangular panels with minimal sound radiation

Author:

LAMANCUSA JOHN1,ESCHENAUER HANS2

Affiliation:

1. Pennsylvania State Univ., University Park

2. Siegen Univ., Germany

Publisher

American Institute of Aeronautics and Astronautics

Reference36 articles.

1. Upper and lower bounds on the design variables also may be imposed such that blower 5 bi _< bypper.Mathematically and numerically,these areusually treated like inequality constraints. The SAPOP program (Structural Analysis Program and Optimization Procedure) [21]was chosen for this problem due to its proven efficiency and utility. This package features a number of optimizer algorithms which can be applied interchangeably to suit the particular demands of a given problem. The particular optimizer used in this study used the hybrid SQP-GRG algorithm [22], which employs the SQP (Sequential Quadratic Programming) search direction and the GRG (Generalized Reduced Gradient) line search. This algorithm features good convergence and is applicable to non-linear problems with large numbers of variables and/or constraints. Other optimizers in the SAPOP package include a SLP (Sequential Linear Programming), SQP, and GRG. For performance comparison, the CONMIN program [23] was also used for a few cases.

2. V21 - 4 2

3. Each case was designed to be dynamically similar,with the initialdesigns all having the same natural frequency of 108 Hz. For the broad band cases, a 90-900 Hz frequency band was used, which encompasses the first five symmetric modes of each plate.

4. The broad band power from 90-900 Hz was then minimized using two different ranges of lower and upper bounds, 1:10 (.894-8.94mm) and 1:4 (1.97-7.87mm). The results are displayed in Figure 4 and demonstrate that wider bounds typically result in lower optimums (13.2 vs 3.4 dB improvement). These cases resulted in an increases in the plate weight of 30% and 27%.

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