NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Comparison of Response Surface and Kriging Models for Multidisciplinary Design OptimizationIn 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 m 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.
Document ID
20040090602
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Simpson, Timothy W.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Korte, John J.
(NASA Langley Research Center Hampton, VA, United States)
Mauery, Timothy M.
(Brigham Young Univ. Provo, UT, United States)
Mistree, Farrokh
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA Paper 98-4755
Report Number: AIAA Paper 98-4755
Funding Number(s)
CONTRACT_GRANT: NAS1-19480
CONTRACT_GRANT: NSF DMI-96-12327
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available