Nonlinear Flutter Test of a Very Flexible Wing
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_211
Reference10 articles.
1. Tang D, Dowell EH (2001) Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings. AIAA J 39(8):1430–1441. https://doi.org/10.2514/2.1484
2. Romeo G, Cestino E, Marzocca P et al (2006) Non-Linear aeroelastic modeling and experiments of flexible wings. In: AIAA 2006-2186. https://doi.org/10.2514/6.2006-2186
3. Britt RT, Ortega D, Tigue JM et al (2012) Wind tunnel test of a very flexible aircraft wing. In: AIAA 2012-1464. https://doi.org/10.2514/6.2012-1464
4. Xie C, Liu Y, Yang C (2012) Static Aeroelastic analysis of very flexible wing based on the 3-d lifting- line theory. In: AIAA 2012-1459. https://doi.org/10.2514/6.2012-1459
5. Xie C, Liu Y, Yang C (2012) Theoretic analysis and experiment on aeroelasticity of very flexible wing. Sci China Technol Sci 55(9):2489–2500. https://doi.org/10.1007/s11431-012-4941-3
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