Reduced-order model for robust aeroelastic control

Author:

Brüderlin ManuelORCID,Hosters Norbert,Behr Marek

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference72 articles.

1. Stickan, B., Johannes, D., Jens, N.: Limit-cylcle-oscillation simulations of AEROSTABIL Windtunnel experiments. In: 17th International forum on aeroelasticity and structural dynamics (IFASD), Saint Petersburg, Russia, 2015

2. Kroll, N., et al.: DLR project digital-X: towards virtual aircraft design and flight testing based on high-fidelity methods. CEAS Aeronaut. J. 7(1), 3–27 (2015). https://doi.org/10.1007/s13272-015-0179-7

3. Lucia, D.J., Beran, P.S., Silva, W.A.: Reduced-order modeling: new approaches for computational physics. Progress Aerosp. Sci. 40(1–2), 51–117 (2004). https://doi.org/10.1016/j.paerosci.2003.12.001

4. Dowell, E.H.: Some recent advances in nonlinear aeroelasticity: fluid-structure interaction in the 21st century. In: 51st AIAA/ASME/-ASCE/AHS/ASC structures, structural dynamics, and materials conference. 3137. American Institute of Aeronautics and Astronautics, (2010). https://doi.org/10.2514/6.2010-3137

5. Widhalm M., et al.: Efficient computation of dynamic stability data with a linearized frequency domain solver. In: Pereira, J. C. F., Sequeira, A. (eds.) European conference on computational fluid dynamics ECCOMAS CFD, Lisbon, Portugal (2010)

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