Abstract
A flying machine either uses a flapping mechanism, a fixed wing or a rotating blade in order to produce lift. While considering fixed wing aircraft or a drone, in order to produce a lift or a decent, the major contributing part is the aileron. An aileron area with respect to the wing is nearly 15%. Rather a discreet movement of aileron, the wing surface can be morphed in order to produce an effect similar to aileron. This research is done to compare and analyze a morphed wing with an aileron-based wing in order to produce the lift and identify maneuvering effects for a drone. Continuous lift force distribution throughout the wing is observed over a range of different wind speeds, and the results are found to be satisfactory.
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References
Babinsky H (2003) How do wings work? www.iop.org/journals/physed
Sofla AYN, Meguid SA, Tan KT, Yeo WK (2010) Shape morphing of aircraft wing: status and challenges. Mater Des 31(3):1284–1292
Budarapu PR, Sudhir Sastry YB, Natarajan R (2016) Design concepts of an aircraft wing: composite and morphing airfoil with auxetic structures. Front Struct Civ Eng 10(4):394–408. https://doi.org/10.1007/s11709-016-0352-z
Li D, Zhao S, Ronch AD, Xiang J, Drofelnik J, Li Y, Zhang L, Wu Y, Kintscher M, Monner HP, Rudenko A, Guo S, Yin W, Kirn J, Storm S, De Breuker R (2018) A review of modelling and analysis of morphing wings. Progr Aerosp Sci 100:46–62. ISSN 0376-0421. https://doi.org/10.1016/j.paerosci.2018.06.002
Ajaj RM, Parancheerivilakkathil MS, Amoozgar M, Friswell MI, Cantwell WJ (2021) Recent developments in the aeroelasticity of morphing aircraft. Prog Aerosp Sci 120. https://doi.org/10.1016/j.paerosci.2020.100682
Muhammed SP, Ajaj RM, Khan KA (2020) A compliant polymorphing wing for small UAVs. Chin J Aeronaut 33(10):2575–2588
Woods BK, Bilgen O, Friswell MI (2014) Wind tunnel testing of the fish bone active camber morphing concept. J Intell Mater Syst Struct 25(7):772–785
Hasse A, Zuest I, Campanile LF (2011) Modal synthesis of belt-rib structures. Proc Inst Mech Eng Part C J Mech Eng Sci 225(3):722–732
Berci M, Toropov VV, Hewson RW, Gaskell PH (2014) Multidisciplinary multifidelity optimisation of a flexible wing aerofoil with reference to a small UAV. Struct Multidiscip Optim 50(4):683–699
Airoldi A, Crespi M, Quaranta G, Sala G (2012) Design of a morphing airfoil with composite chiral structure. J Aircr 49(4):1008–1019
Li D, Zhao S, da Ronch A et al (2018) A review of modelling and analysis of morphing wings. Prog Aerosp Sci 100:46–62
Communier D, Botez RM, Wong T (2020) Design and validation of a new morphing camber system by testing in the price—Païdoussis subsonic wind tunnel. Aerospace 7(3):23
Meguid S, Su Y, Wang Y (2017) Complete morphing wing design using flexible-rib system. Int J Mech Mater Des 13(1):159–171
Chanzy Q, Keane A (2018) Analysis and experimental validation of morphing UAV wings. Aeronaut J 122(1249):390–408
Kudva JN, Martin CA, Scherer LB et al (1999) Overview of the DARPA/AFRL/NASA smart wing program. In: Smart structures and materials 1999 industrial and commercial applications of smart structures technologies. International Society for Optics and Photonics, pp 230–236
Lobo do Vale J, Raffaelli J, Suleman A (2021) Experimental validation and evaluation of a coupled twist-camber morphing wing concept. Appl Sci 11:10631.https://doi.org/10.3390/app112210631
Cody L, Kelly C, Shaaban A (2012) Use of XFOIL in design of camber-controlled morphing UAVs. Comput Appl Eng Educ 20:673–680
Critzos CC, Heyson HH, Boswinkle Jr RW (1955) Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees (No. NACA-TN-3361)
Ryaciotaki-Boussalis H, Guillaume D (2015) Computational and experimental design of a fixed-wing UAV. In: Valavanis K, Vachtsevanos G (eds) Handbook of unmanned aerial vehicles. Springer, Dordrecht. https://doi.org/10.1007/978-90-481-9707-1_121
Rao D (2020) Design and analysis of fixed-wing UAV. The print has aerodynamic, structural and stability analysis of a Fixed-Wing UAV
Ghalandari M, Mahariq I, Ghadak F, Accouche O, Jarad F (2021) Aeroelastic optimization of the high aspect ratio wing with aileron. Comput Mater Continua 70. https://doi.org/10.32604/cmc.2022.020884
Wu SF, Grimble MJ, Breslin SG (1997) Quantitative feedback theory for lateral robust flight control systems design. 4. TITLE AND SUBTITLE, 235
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Thakur, A., Doss, A.S.A., Schilberg, D. (2023). Design and Analysis of Morphed Wings. In: Sethuraman, B., Jain, P., Gupta, M. (eds) Recent Advances in Mechanical Engineering. STAAAR 2022. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-99-2349-6_27
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DOI: https://doi.org/10.1007/978-981-99-2349-6_27
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