Numerical modeling and simulation represent the current paradigm in science that aims at high fidelity and cost effectiveness. Consequently, model reduction techniques have been developed to meet the requirements, while at the same time to minimize the size and intricacy of the model. Previously, a novel parametric reduced-order model (PROM) technique for linear systems was developed based on the so-called dynamic eigen decomposition (DED) and modally equivalent perturbed system (MEPS). The main advantage of the scheme is that it isolates all the parameter changes into the right-hand side forcing term, thereby allowing the perturbed system to be analyzed through the ordinary differential equation with constant coefficients and varying forcing terms. It was shown that when the parameter variation is limited to a finite dimension, the scheme yields an exceptionally accurate reduced-order model for a wide range of parameter values. However, although the theory of the MEPS is valid for all ranges of the variations, in certain situations its frequency snapshots may lack the spatial richness necessary for capturing the full spectrum of the solution subspace.
To address this issue and seek for a remedy, Dr. Taehyoun (John) Kim at the Department of Mechanical Engineering from National University of Singapore (currently at Pegase Avtech in Washington) critically reviewed the original method with the aim of improving it and making it numerically robust for parameter variations that propagate in a larger dimensional domain and possibly the entire domain. The author effected the aforementioned changes by expanding the original first-order MEPS to a higher-order MEPS (HOMEPS) adding the extra higher-order terms in the formulation. His work is currently published in the International Journal for Numerical Methods in Engineering.
Interestingly, the author showed that when expressed in powers of incremental matrices, the new formula becomes identical to a truncated Neumann series, which in turn can be replaced by a Taylor series of the same order without affecting the modal space that it represents. It is well known that the Neumann series converges or diverges depending on the norm of the incremental matrix. On the other hand, the HOMEPS always converges in that it improves the basis vectors as more of the higher-order terms are added. The attached figures illustrate graphically the fundamental difference in the two matrix approximations. Whereas in the first plot, the HOMEPS converges in both magnitude and direction, in the second, it converges in direction but diverges in magnitude.
In summary, the study extended the previously presented MEPS formula to account for parameter variations in a larger domain and the global domain by deriving and adding the higher-order terms. The improved PROM scheme was demonstrated using a computational fluid dynamics model of unsteady air flow around a 2D airfoil with Mach variation at subsonic speeds. Predictably, it was shown that the results of the higher-order PROM match very well those of the full-order models for a wide range of Mach numbers improving significantly over the previous PROM.


Dr. John T. Kim worked for Boeing Commercial Aircraft, Seattle, for seventeen years. Prior to this, he was a research associate at Georgia Institute of Technology. His areas of specialty are structural dynamics, fluid-structure-control interaction (a.k.a., aeroservoelasticity), flight flutter and limit cycle oscillation (LCO) testing methods, system identification and reduced-order modeling of large-scaled dynamic systems, unsteady aerodynamics, and composite structures. At Boeing, he developed innovative computational and experimental tools to enhance accurate and rapid estimation of dynamic loads, flutter and control laws, all of which are essential in design and analysis of modern aircraft structures. In 2003 he was awarded the Best Paper Award at the 5th BTEC (Boeing Technological Conference) for his work on reduced-order aerodynamic and aeroelastic modeling. Since 2005 he has taught the short course, “Computational Methods in Aeroelasticity” at AIAA Conf., Boeing Ed Wells, National Aerospace Laboratory (NAL) in Bangalore, India, NASA Langley, National University of Singapore, Korea Aerospace Industries (KAI), Seoul National University, South Korea, and Royal Melbourne Institute of Technology (RMIT), Australia. From 2013 till 2017 he taught at National University of Singapore in the Department of Mechanical Engineering. In 2017 he founded Pegase Avtech and since then has been working as an engineering consultant for aviation companies in Europe and South Korea. He is also currently teaching at University of Washington.
Dr. Kim’s latest research is focused on characteristic and parametric nonlinear vector space which can lead to significant reductions in CPU time and complexity of nonlinear system analysis. He is an Associate Fellow of American Institute of Aeronautics and Astronautics and has one US patent on system identification. He earned his BA from Ajou University, South Korea, MS from University of Texas at Austin, USA, and Ph.D. in Aeronautics and Astronautics from Massachusetts Institute of Technology, USA.
Email: [email protected]
Reference
T. Kim. Higher-order modal transformation for reduced-order modeling of linear systems undergoing global parametric variations. International Journal for Numerical Methods in Engineering 2018;volume 115: page 1477–1498.
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