Comparison of response surface and kriging models for multidisciplinary design optimization

Timothy W. Simpson, Timothy M. Mauery, John J. Korte, Farrokh Mistree

Research output: Contribution to conferencePaperpeer-review

369 Scopus citations

Abstract

In this paper, we compare and contrast the use of second-order response surface models and kriging models for approximating non-random, deterministic computer analyses. After reviewing the response surface method for constructing polynomial approximations, kriging is presented as an alternative approximation method for the design and analysis of computer experiments. Both methods are applied to the multidisciplinary design of an aerospike nozzle which consists of a computational fluid dynamics model and a finite-element model. Error analysis of the response surface and kriging models is performed along with a graphical comparison of the approximations, and four optimization problems are formulated and solved using both sets of approximation models. The second-order response surface models and kriging models—using a constant underlying global model and a Gaussian correlation function—yield comparable results.

Original languageEnglish (US)
Pages381-391
Number of pages11
DOIs
StatePublished - 1998
Event7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1998 - St. Louis, United States
Duration: Sep 2 1998Sep 4 1998

Other

Other7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 1998
Country/TerritoryUnited States
CitySt. Louis
Period9/2/989/4/98

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Mechanical Engineering

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