A Multibody Dynamics Approach to Study an Insect-Wing Structure
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-16-3239-6_12
Reference13 articles.
1. Altenbuchner, C., Hubbard Jr., J.E.: Modern Flexible Multi-Body Dynamics Modeling Methodology for Flapping Wing Vehicles. Elsevier (2018)
2. Tuan, A., Han, J.: Wing flexibility effects on the flight performance of an insect-like flapping-wing micro-air vehicle. Aerosp. Sci. Technol. 79, 468–481 (2018). https://doi.org/10.1016/j.ast.2018.06.007
3. Verstraete, M.L., Roccia, B.A., Mook, D.T., Preidikman, S.: A co-simulation methodology to simulate the nonlinear aeroelastic behavior of a folding-wing concept in different flight configurations. Nonlinear Dyn. 98(2), 907–927 (2019). https://doi.org/10.1007/s11071-019-05234-9
4. Hara, R.P.O., Palazotto, A.N.: The morphological characterization of the forewing of the Manduca sexta species for the application of biomimetic flapping wing micro air vehicles, vol. 046011. https://doi.org/10.1088/1748-3182/7/4/046011
5. Bomphrey, R.J., Lawson, N.J., Harding, N.J., Taylor, G.K., Thomas, A.L.R.: The aerodynamics of Manduca sexta: Digital particle image velocimetry analysis of the leading-edge vortex. J. Exp. Biol. 208(6), 1079–1094 (2005). https://doi.org/10.1242/jeb.01471
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