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A Versatile Nonlinear Method for Predictive ModelingAs computational fluid dynamics techniques and tools become widely accepted for realworld practice today, it is intriguing to ask: what areas can it be utilized to its potential in the future. Some promising areas include design optimization and exploration of fluid dynamics phenomena (the concept of numerical wind tunnel), in which both have the common feature where some parameters are varied repeatedly and the computation can be costly. We are especially interested in the need for an accurate and efficient approach for handling these applications: (1) capturing complex nonlinear dynamics inherent in a system under consideration and (2) versatility (robustness) to encompass a range of parametric variations. In our previous paper, we proposed to use first-order Taylor expansion collected at numerous sampling points along a trajectory and assembled together via nonlinear weighting functions. The validity and performance of this approach was demonstrated for a number of problems with a vastly different input functions. In this study, we are especially interested in enhancing the method's accuracy; we extend it to include the second-orer Taylor expansion, which however requires a complicated evaluation of Hessian matrices for a system of equations, like in fluid dynamics. We propose a method to avoid these Hessian matrices, while maintaining the accuracy. Results based on the method are presented to confirm its validity.
Document ID
20150019483
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Liou, Meng-Sing
(NASA Glenn Research Center Cleveland, OH United States)
Yao, Weigang
(Queens Univ. Belfast, United Kingdom)
Date Acquired
October 20, 2015
Publication Date
June 22, 2015
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN24042
Report Number: GRC-E-DAA-TN24042
Meeting Information
Meeting: Computational Fluid Dynamic Conference
Location: Dallas, TX
Country: United States
Start Date: June 22, 2015
End Date: June 26, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 794072.02.03.05.05
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
nonlinear modeling
Hessian approximation
piecewise quadratic expansion
computational fluid dynamics
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