Aeroelastic scaling of flying demonstrators: mode tracking technique

Joan Mas Colomer; Nathalie Bartoli; Thierry Lefebvre; Joseph Morlier

doi:10.1051/meca/2021051

All issues

Volume 23 (2022)

Mechanics & Industry, 23 (2022) 2

References

Open Access

Issue		Mechanics & Industry Volume 23, 2022


Article Number		2
Number of page(s)		12
DOI		https://doi.org/10.1051/meca/2021051
Published online		21 January 2022

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M. French, An application of structural optimization in wind tunnel model design, in: 31st Structures, Structural Dynamics and Materials Conference, American Institute of Aeronautics and Astronautics, Long Beach, California (1990) [Google Scholar]
M. French, F.E. Eastep, Aeroelastic model design using parameter identification, J. Aircraft 33, 198–202 (1996) [Google Scholar]
P. Pereira, L. Almeida, A. Suleman, V. Bond, R. Canfield, M. Blair, Aeroelastic scaling and optimization of a joined-wing aircraft concept, in: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, 2007 [Google Scholar]
V.L. Bond, R.A. Canfield, A. Suleman, M. Blair, Aeroelastic scaling of a joined wing for nonlinear geometric stiffness, AIAA J. 50, 513–522 (2012) [Google Scholar]
J. Richards, A. Suleman, R. Canfield, M. Blair, Design of a scaled RPV for investigation of gust response of joined-wing sensorcraft, in: 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Palm Springs, California, 2009 [Google Scholar]
A. Ricciardi, R. Canfield, M. Patil, N. Lindsley, Nonlinear aeroelastic scaling of a joined wing aircraft, in: 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, in American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, 2012 [Google Scholar]
A.P. Ricciardi, C.A.G. Eger, R.A. Canfield, M.J. Patil, Nonlinear aeroelastic-scaled-model optimization using equivalent static loads. J. Aircraft 51, 1842–1851 (2014) [Google Scholar]
A.P. Ricciardi, R.A. Canfield, M.J. Patil, N. Lindsley, Nonlinear aeroelastic. J. Aircraft 53, 20–32 (2016) [CrossRef] [Google Scholar]
J. Mas Colomer, N. Bartoli, T. Lefebvre, et al. Similarity maximization of a scaled aeroelastic flight demonstrator via multidisciplinary optimization, in: 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Grapevine, Texas, 2017 [Google Scholar]
C. Spada, F. Afonso, F. Lau, A. Suleman, Nonlinear aeroelastic scaling of high aspect-ratio wings. Aerospace Sci. Technol. 63, 363–371 (2017) [Google Scholar]
T.R. Brooks, G.K.W. Kenway, J.R.R.A. Martins, Benchmark aerostructural models for the study of transonic aircraft wings. AIAA J. 56, 2840–2855 (2018) [CrossRef] [Google Scholar]
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T. Marwala, Finite element model updating using computational intelligence techniques: applications to structural dynamics, Springer Science & Business Media (2010) [Google Scholar]
J. Mas Colomer Aeroelastic similarity of a flight demonstrator via multidisciplinary optimization, Ph.D. thesis, Doctorat de l’Université de Toulouse délivré par: l’Institut Supérieur de l’Aéronautique et de l’Espace (ISAE), 2018 [Google Scholar]
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D.F. Giraldo, A structural health monitoring framework for civil structures, Ph.D. thesis, Washington University, Saint Louis, Missouri, 2006 [Google Scholar]
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J. Mas Colomer, N. Bartoli, T. Lefebvre, J.R. R.A. Martins, J. Morlier, An MDO-based methodology for static aeroelastic scaling of wings under non-similar flow, Struct. Multidiscipl. Optim. 63, 1045–1061 (2021) [CrossRef] [Google Scholar]
C.W. MacCormick, The NASTRAN User’s Manual:(level 15), National Aeronautics and Space Administratio, 1972 [Google Scholar]
J. Mas Colomer, N. Bartoli, T. Lefebvre, J.R. Martins, J. Morlier, Aeroelastic scaling of flying demonstrator: flutter matching, Mech. Ind. 22, 42 (2021) [CrossRef] [EDP Sciences] [Google Scholar]
A. Girard, N. Roy, in: Structural dynamics in industry, John Wiley & Sons, 2010, Vol. 7 [Google Scholar]
T.C.S. Rendall, C.B. Allen, Unified fluid-structure interpolation and mesh motion using radial basis functions, Int. J. Numer. Methods Eng. 74, 1519–1559 (2008) [Google Scholar]

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[1] R.L. Bisplinghoff, H. Ashley, R.L. Halfman, Aeroelasticity, Courier Corporation (1996) [Google Scholar]

[2] C. Scruton, N. Lambourne, Similarity requirements for flutter model testing, in: E.C. Pike (Ed.), Manuel on Aeroelasticity, Vol. IV of AGARD, 1971, Chap. 6, pp. 1–26 [Google Scholar]

[3] M. French, An application of structural optimization in wind tunnel model design, in: 31st Structures, Structural Dynamics and Materials Conference, American Institute of Aeronautics and Astronautics, Long Beach, California (1990) [Google Scholar]

[4] M. French, F.E. Eastep, Aeroelastic model design using parameter identification, J. Aircraft 33, 198–202 (1996) [Google Scholar]

[5] P. Pereira, L. Almeida, A. Suleman, V. Bond, R. Canfield, M. Blair, Aeroelastic scaling and optimization of a joined-wing aircraft concept, in: 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, 2007 [Google Scholar]

[6] V.L. Bond, R.A. Canfield, A. Suleman, M. Blair, Aeroelastic scaling of a joined wing for nonlinear geometric stiffness, AIAA J. 50, 513–522 (2012) [Google Scholar]

[7] J. Richards, A. Suleman, R. Canfield, M. Blair, Design of a scaled RPV for investigation of gust response of joined-wing sensorcraft, in: 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Palm Springs, California, 2009 [Google Scholar]

[8] A. Ricciardi, R. Canfield, M. Patil, N. Lindsley, Nonlinear aeroelastic scaling of a joined wing aircraft, in: 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, in American Institute of Aeronautics and Astronautics, Honolulu, Hawaii, 2012 [Google Scholar]

[9] A.P. Ricciardi, C.A.G. Eger, R.A. Canfield, M.J. Patil, Nonlinear aeroelastic-scaled-model optimization using equivalent static loads. J. Aircraft 51, 1842–1851 (2014) [Google Scholar]

[10] A.P. Ricciardi, R.A. Canfield, M.J. Patil, N. Lindsley, Nonlinear aeroelastic. J. Aircraft 53, 20–32 (2016) [CrossRef] [Google Scholar]

[11] J. Mas Colomer, N. Bartoli, T. Lefebvre, et al. Similarity maximization of a scaled aeroelastic flight demonstrator via multidisciplinary optimization, in: 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Grapevine, Texas, 2017 [Google Scholar]

[12] C. Spada, F. Afonso, F. Lau, A. Suleman, Nonlinear aeroelastic scaling of high aspect-ratio wings. Aerospace Sci. Technol. 63, 363–371 (2017) [Google Scholar]

[13] T.R. Brooks, G.K.W. Kenway, J.R.R.A. Martins, Benchmark aerostructural models for the study of transonic aircraft wings. AIAA J. 56, 2840–2855 (2018) [CrossRef] [Google Scholar]

[14] M. Friswell, J.E. Mottershead, in: Finite element model updating in structural dynamics, Springer Science & Business Media (2013), Vol. 38 [Google Scholar]

[15] T. Marwala, Finite element model updating using computational intelligence techniques: applications to structural dynamics, Springer Science & Business Media (2010) [Google Scholar]

[16] J. Mas Colomer Aeroelastic similarity of a flight demonstrator via multidisciplinary optimization, Ph.D. thesis, Doctorat de l’Université de Toulouse délivré par: l’Institut Supérieur de l’Aéronautique et de l’Espace (ISAE), 2018 [Google Scholar]

[17] T. Pires, Linear Aeroelastic Scaling of a Joined Wing Aircraft, Instituto Superior Tecnico, TU Lisbon, 2014 [Google Scholar]

[18] B. Prananta, T. Kanakis, J. Vankan, R. van Houten, Model updating of finite element model using optimisation routine, Aircraft Eng. Aerospace Technol. 88, 665–675 (2016) [Google Scholar]

[19] A. Gupta, C.P. Moreno, H. Pfifer, B. Taylor, G.J. Balas, Updating a finite element based structural model of a small flexible aircraft, in: AIAA Modeling and Simulation Technologies Conference, 2015, p. 0903 [Google Scholar]

[20] R.J. Allemang, D.L. Brown, A correlation coefficient for modal vector analysis, in: Proceedings of the 1st international modal analysis conference, Vol. 1, SEM Orlando, 1982, pp. 110–116 [Google Scholar]

[21] D.F. Giraldo, A structural health monitoring framework for civil structures, Ph.D. thesis, Washington University, Saint Louis, Missouri, 2006 [Google Scholar]

[22] J. Morlier, A. Basile, A. Chiplunkar, M. Charlotte, An ego-like optimization framework for sensor placement optimization in modal analysis. Smart Mater. Struct. 27, 075004 (2018) [CrossRef] [Google Scholar]

[23] T.S. Kim, Y.Y. Kim, Mac-based mode-tracking in structural topology optimization. Comput. Struct. 74, 375–383 (2000) [CrossRef] [Google Scholar]

[24] T. Ting, T.L.C. Chen, W.J. Twomey, An automated mode tracking strategy (dynamic structural analysis of helicopterstructures), AIAA J. 33, 183–185 (1995) [CrossRef] [Google Scholar]

[25] J.C. Vassberg, M.A. DeHaan, S.M. Rivers, R.A. Wahls, Development of a common research model for applied CFD validationstudies, AIAA paper 6919, 2008 [Google Scholar]

[26] M.J. Powell, A direct search optimization method that models the objective and constraint functions by linear interpolation, in: Advances in optimization and numerical analysis, Springer, 1994, pp. 51–67 [CrossRef] [Google Scholar]

[27] J. Mas Colomer, N. Bartoli, T. Lefebvre, J.R. R.A. Martins, J. Morlier, An MDO-based methodology for static aeroelastic scaling of wings under non-similar flow, Struct. Multidiscipl. Optim. 63, 1045–1061 (2021) [CrossRef] [Google Scholar]

[28] C.W. MacCormick, The NASTRAN User’s Manual:(level 15), National Aeronautics and Space Administratio, 1972 [Google Scholar]

[29] J. Mas Colomer, N. Bartoli, T. Lefebvre, J.R. Martins, J. Morlier, Aeroelastic scaling of flying demonstrator: flutter matching, Mech. Ind. 22, 42 (2021) [CrossRef] [EDP Sciences] [Google Scholar]

[30] A. Girard, N. Roy, in: Structural dynamics in industry, John Wiley & Sons, 2010, Vol. 7 [Google Scholar]

[31] T.C.S. Rendall, C.B. Allen, Unified fluid-structure interpolation and mesh motion using radial basis functions, Int. J. Numer. Methods Eng. 74, 1519–1559 (2008) [Google Scholar]