Investigation on buckling response of the aircraft’s wing using finite-element method

References

• Abbishek, R., B. Ravi Kumar, and H. Sankara Subramanian. 2017 August. “Fatigue Analysis and Design Optimization of Aircraft’s Central Fuselage.” IOP Conference Series: Materials Science and Engineering 225 12031. doi:10.1088/1757-899X/225/1/012031.
   Google Scholar
• Barkanov, E., E. Eglitis, F. Almeida, M. C. Bowering, and G. Watson. 2016. “Optimal Design of Composite Lateral Wing Upper Covers. Part II: Nonlinear Buckling Analysis.” Aerospace Science and Technology 51: 87–95. doi:10.1016/j.ast.2016.01.020.
   Web of Science ®Google Scholar
• Barkanov, E., O. Ozoliņš, E. Eglitis, F. Almeida, M. C. Bowering, and G. Watson. 2014. “Optimal Design of Composite Lateral Wing Upper Covers. Part I: Linear Buckling Analysis.” Aerospace Science and Technology 38: 1–8. doi:10.1016/j.ast.2014.07.010.
   Web of Science ®Google Scholar
• Gallman, J. W., S. C. Smith, and I. M. Kroo. 1993. “Optimization of Joined-Wing Aircraft.” Journal of Aircraft 30 (6): 897–905. doi:10.2514/3.46432.
   Web of Science ®Google Scholar
• Gliszczyński, A., and T. Kubiak. 2017. “Load-Carrying Capacity of Thin-Walled Composite Beams Subjected to Pure Bending.” Thin-Walled Structures 115 (115): 76–85. doi:10.1016/j.tws.2017.02.009.
   Google Scholar
• Hoogervorst, J. E. K., and A. Elham. 2017. “Wing Aerostructural Optimization Using the Individual Discipline Feasible Architecture.” Aerospace Science and Technology 65. 90–99. Elsevier Masson. doi:10.1016/J.AST.2017.02.012.
   Web of Science ®Google Scholar
• Hughes, T. J. R., and W. K. Liu. 1981. “Nonlinear Finite Element Analysis of Shells: Part I. Three-Dimensional Shells.” Computer Methods in Applied Mechanics and Engineering 26(3):331–362. Elsevier. doi:10.1016/0045-7825(81)90121-3.
   Web of Science ®Google Scholar
• Kolanu, N. R., G. Raju, and M. Ramji. 2018.“Experimental and Numerical Studies on the Buckling and Post-Buckling Behavior of Single Blade-Stiffened CFRP Panels.” Composite Structures. doi:10.1016/j.compstruct.2018.05.015.
   PubMedGoogle Scholar
• Kong, C., H. Park, Y. Kim, and K. Kang. 2007. “Structural Design on Wing of a Small Scale Wig Vehicle with Carbon/Epoxy and Foam Sandwich Composite Structure.” 16th International Conference on Composite Materials, 1–8.
   Google Scholar
• Kumar, R., and S. Deol. 2016. “Nonlocal Buckling Analysis of Single-Walled Carbon Nanotube Using Differential Transform Method (DTM).” International Journal of Science and Research (IJSR) ISSN (Online Index Copernicus Value Impact Factor 5 (3). www.ijsr.net.
   Google Scholar
• Novitskaya, E., C. J. Ruestes, M. M. Porter, V. A. Lubarda, M. A. Meyers, and J. McKittrick. 2017. “Reinforcements in Avian Wing Bones: Experiments, Analysis, and Modeling.” Journal of the Mechanical Behavior of Biomedical Materials 76. 85–96. Elsevier. doi:10.1016/J.JMBBM.2017.07.020.
   PubMed Web of Science ®Google Scholar
• Paul, A., and S. P. George. 2014. “Buckling Analysis of Wing Upper Skin Panels of a Transport Aircraft.” International Journal of Science, Engineering and Technology Research (IJSETR) 3 (10): 2868–2872.
   Google Scholar
• Rajappan, R., and V. Pugazhenthi. 2013. “Finite Element Analysis of Aircraft Wing Using Composite Structure.” The International Journal of Engineering and Science (IJES) 2 (2): 74–80.
   Google Scholar
• Ravi Kumar, B. 2017a. “Mechanical Buckling Analysis of Single-Walled Carbon Nanotube with Nonlocal Effects.” Journal of Nano Research 48: 85–94. doi:10.4028/www.scientific.net/JNanoR.48.85.
   Web of Science ®Google Scholar
• Ravi Kumar, B. 2017b. “Nonlocal Vibration Analysis of Fluid Conveying Single-Walled Carbon Nanotube with Magnetic Effects.” Rasayan Journal of Chemistry 10: 2. doi:10.7324/RJC.2017.1021669.
   Google Scholar
• Ravi Kumar, B., S. Mano, and H. S. Subramanian. 2017. “Vibration Analysis and Design Modification of Automobile Muffler.” Journal of Advanced Research in Dynamical and Control Systems 11 (Special Issue): 99–107.
   Google Scholar
• Saranprabhu, M. K., B. Ravi Kumar, and V. M. Sreehari. 2017. “Aero-Thermodynamic Analysis of a Supersonic Aircraft.” Journal of Advanced Research in Dynamical and Control Systems 11 (Special issue): 120–127.
   Google Scholar
• Shen, H.-S., Y. Xiang, F. Lin, and D. Hui. 2017. “Buckling and Postbuckling of Functionally Graded Graphene-Reinforced Composite Laminated Plates in Thermal Environments.” Composites Part B: Engineering 119: 67–78. doi:10.1016/j.compositesb.2017.03.020.
   Web of Science ®Google Scholar
• Sivakumar, V., G. Bharath Kumar, and A. Gautham. 2015. “Crack Initiation Study on Aircraft Composite Rib with Semi-Elliptical Surface Flaw.” Journal of Failure Analysis and Prevention 15(6):906–914. Springer US. doi:10.1007/s11668-015-0029-2.
   Web of Science ®Google Scholar
• Sreehari, V. M., and D. K. Maiti. 2015. “Buckling and Post Buckling Analysis of Laminated Composite Plates in Hygrothermal Environment Using an Inverse Hyperbolic Shear Deformation Theory.” Composite Structures 129: 250–255. doi:10.1016/j.compstruct.2015.04.010. October.
   Web of Science ®Google Scholar
• Sreehari, V. M., B. Ravi Kumar, and D. K. Maiti. 2017. “Structural Analysis Using Shear Deformation Theories Having Nonpolynomial Nature: A Review.” International Journal of Applied Engineering Research 12: 20.
   Google Scholar
• Starnes, J. H., Jr., and R. T. Haftka. 1979. “Preliminary Design of Composite Wings for Buckling, Strength, and Displacement Constraints.” Journal of Aircraft 16 (8): 564–570. doi:10.2514/3.58565.
   Web of Science ®Google Scholar
• York, C. B., and F. W. Williams. 1998. “Aircraft Wing Panel Buckling Analysis: Efficiency by Approximations.” Computers & Structures 68 (6): 665–676. doi:10.1016/S0045-7949(98)00050-9.
   Web of Science ®Google Scholar