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. 2020 Apr 15;13(8):1856. doi: 10.3390/ma13081856

Figure 9.

Figure 9

Example of infrared results for morphed wing demonstrator without aileron [34]. Figure 9 Reprinted from Chinese Journal of Aeronautics, Vol. 30 (1), Koreanski, A.; Gabor, O.S.; Acotto, J.; Brianchon, G.; Portier, G., Botez, R.M.; Mamou, M.; Mebarki, Y., Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speed, Part. II – Experimental validation using Infra-red transition measurement from wind tunnel tests, 164–174, 2017, open access.