Aerodynamic Shape Optimization and the Effect of Morphing Winglet-Induced Tip Vortex Structure on the UAS-S45
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-45321-2_7
Reference62 articles.
1. Ameduri S, Concilio A (2020) Morphing wings review: aims, challenges, and current open issues of a technology. Proc Inst Mech Eng Part C J Mech Eng Sci 237(18). https://doi.org/10.1177/0954406220944423
2. Arena M, Concilio A, Pecora R (2019) Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance. Aerosp Sci Technol 86:215–235
3. Aubeelack H, Botez RM (2019) Simulation study of the aerodynamic force distributions on the Uas-S45 Baalam wing with an upswept blended winglet. INCAS Bull 11:21–38
4. Barbarino S, Bilgen O, Ajaj RM, Friswell MI, Inman DJ (2011) A review of morphing aircraft. J Intell Mater Syst Struct 22:823–877
5. Bashir M, Longtin-Martel S, Botez RM, Wong T (2021) Aerodynamic design optimization of a morphing leading edge and trailing edge airfoil–application on the UAS-S45. Appl Sci 11:1664
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