Open Access
Issue
MATEC Web Conf.
Volume 198, 2018
2018 Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2018)
Article Number 03002
Number of page(s) 5
Section Fluid Mechanics and Modeling
DOI https://doi.org/10.1051/matecconf/201819803002
Published online 12 September 2018
  1. M. Ghoreyshi, K. J. Badcock, A. D. Ronch, et al., J Aircr, Framework for establishing limits of tabular aerodynamic models for flight dynamics analysis 48, 42–55 (2011) [CrossRef] [Google Scholar]
  2. M. Ghoreyshi, A. Jirasek, R. M. Cummings, AIAA J, Computational investigation into the use of response functions for aerodynamic-load modeling 50, 1314–1327 (2012) [CrossRef] [Google Scholar]
  3. A. J. Mccracken, D. J. Kennett, K. J. Badcock, et al., AIAA Paper 2013-4978, Assessment of tabular models using CFD (2013) [Google Scholar]
  4. M. Ghoreyshi, A. Jirasek, R. M. Cummings, Prog Aerosp Sci, Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics 71, 167–217 (2014) [CrossRef] [Google Scholar]
  5. A. D. Ronch, K. J. Badcock, A. Khrabrov, et al., AIAA Paper 2011-6524, Modeling of unsteady aerodynamic loads (2011) [Google Scholar]
  6. D. J. Lucia, P. S. Beran, W. A. Silva, Prog Aerosp Sci, Reduced-order modeling: New approaches for computational physics 40, 51–117 (2004) [CrossRef] [Google Scholar]
  7. S. Boyd, L. O. Chua, C. A. Desoer, Ima Journal of Mathematical Control and Information, Analytical foundations of Volterra series 1, 243–282 (1984) [CrossRef] [Google Scholar]
  8. T. Skujins, C. Cesnik, AIAA Paper 2010-8127, Reduced-order modeling of hypersonic vehicle unsteady aerodynamics (2010) [Google Scholar]
  9. W. A. Silva, AIAA Paper 1999-1262, Reduced-order models based on linear and nonlinear aerodynamic impulse responses (1999) [Google Scholar]
  10. M. Balajewicz, E. Dowell, J Aircr, Reduced-order modeling of flutter and limit-cycle oscillations using the sparse Volterra series 49, 1803–1812 (2012) [CrossRef] [Google Scholar]
  11. W. A. Silva, J Aircr, Application of nonlinear systems theory to transonic unsteady aerodynamic responses 30, 660–668 (1993) [CrossRef] [Google Scholar]
  12. M. Balajewicz, F. Nitzsche, D. Feszty, AIAA Paper 2009-2319, Reduced order modeling of nonlinear transonic aerodynamics using a pruned Volterra series (2009) [Google Scholar]
  13. C. M. Cheng, Z. K. Peng, W. M. Zhang, et al., Nonlinear Dyn, Wavelet basis expansion-based Volterra kernel function identification through multilevel excitations 76, 985–999 (2014) [CrossRef] [Google Scholar]
  14. R. J. Prazenica, A. J. Kurdila, Nonlinear Dyn, Multiwavelet constructions and Volterra kernel identification 43, 277–310 (2006) [CrossRef] [Google Scholar]
  15. M. Schetzen, The Volterra and Wiener theories of nonlinear systems (2006) [Google Scholar]
  16. S. Boyd, L. O. Chua, IEEE Trans Circ Syst, Fading memory and the problem of approximating nonlinear operators with Volterra series 32, 1150–1161 (1985) [CrossRef] [Google Scholar]
  17. M. Brenner, Y. Jiang, Y. S. Xu, Adv Comput Math, Multiparameter regularization for Volterra kernel identification via multiscale collocation methods 31, 421–455 (2009) [CrossRef] [Google Scholar]
  18. J. W. Xiang, X. F. Chen, Z. J. He, et al., Comput Mech, A new wavelet-based thin plate element using B-spline wavelet on the interval 41, 243–255 (2008) [Google Scholar]
  19. L. Tronchin, J Audio Eng Soc, The emulation of nonlinear time-invariant audio systems with memory by means of Volterra series 60, 984–996 (2012) [Google Scholar]
  20. E. Morelli, S. Derry, M. Smith, AIAA Paper 2005-5921, Aerodynamic parameter estimation for the X-43a (Hyper-X) from flight data (2005) [Google Scholar]

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