Response surface estimation and refinement in collaborative optimization

Author(s):  
I. Sobieski ◽  
V. Manning ◽  
I. Kroo
AIAA Journal ◽  
2000 ◽  
Vol 38 ◽  
pp. 1931-1938 ◽  
Author(s):  
I. P. Sobieski ◽  
I. M. Kroo

AIAA Journal ◽  
10.2514/2.847 ◽  
2000 ◽  
Vol 38 (10) ◽  
pp. 1931-1938 ◽  
Author(s):  
I. P. Sobieski ◽  
I. M. Kroo

Author(s):  
Zhe Jiang ◽  
Weicheng Cui ◽  
Xiaoping Huang

In the traditional design of a Truss Spar, designers usually choose different discipline as major concentration in different design phases. The coupling effect among disciplines can hardly be accounted for. Multidisciplinary design optimization has been proved to be an effective tool for the design of complex engineering systems, which takes all disciplines into account at the same time and exploit coupling effect among disciplines, thereby achieving the optimal system solution. In this paper, a multidisciplinary optimization scheme for a Truss Spar is firstly developed and the Truss Spar is decomposed into four modules: weight module, hydrodynamic module, structure module and stability module. Response surface method is used to replace the high-fidelity analysis to perform the approximate mathematical models of the objective function/constraints as a function of design variables. In order to enhance the accuracy of the predicted optimum, the response surface models are continuously updated using the information obtained from the numerical simulation of latest iterative results. Finally, an optimal design solution, which satisfies all the constraints, is obtained using collaborative optimization. The characteristics of the optimized design solution including hull weight, heave response, stability performance and strength of the bottom deck, are much improved comparing with traditional design.


2013 ◽  
Vol 300-301 ◽  
pp. 99-103
Author(s):  
Ying Liu ◽  
Hong Xin Zhang ◽  
Kai Yin

The technology of multidisciplinary design optimization was elaborated, and the structure principle and dynamic model of HCPE were briefly presented. Based on the minimum volume, the collaborative optimization model of crank-link mechanism was constructed. The approximate response surface models of connecting rod and crankshaft were established by means of ANSYS calculation. By combined with iSIGHT software, the collaborative optimization system was realized, and the calculation speed was improved. The optimized volume decreased by 0.803% under the premise that couldn't change the crankshaft counterbalance. So the mass of the engine is reduced and the performance is improved.


Sign in / Sign up

Export Citation Format

Share Document