Abstract
The present analysis is based upon evaluation and optimization of the structural behavior of wings used in airplanes, as given by advanced material and transport aircraft structure. The main goal is to reduce mass and volume cum the stress and deformation in the plane geometry. The main focus of the analysis is on the factor of safety or level of safety, which is optimized to remain constant for both standard and new model. The analysis of the wing is kept organized only as far as structural and stress analysis is concerned. The aerodynamics analysis can be done for this geometry.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Jweeg, M.J., Abid-Aun, S.H.: Optimization of Light Weight Aircraft Wing Structure. Journal of Engineering & Development, Vol. 12, No. 1, March (2008).
Vinson, J.R.: Optimum Design of Composite Honeycomb Sandwich Panels Subjected to Uniaxial Compression. University of Delaware, AIAA Journal, Vol. 24, No. 10, October 1986, p. 1690–1696.
Iyengar, N.G.R., Joshi, S.P.: Optimal Design of Antisymmetric Laminated Composite Plates. Journal of Aircraft, Vol. 23, No. 5, May 1986, pp. 359–360.
Guo, S.J., Banerjee, J.R., Cheung, C.W.: The effect of laminate lay-up on the flutter speed of composite wings. Proceedings of the Institution of Mechanical Engineers, Part G: journal of aerospace engineering, Vol. 217, No. 3, 2003, pp. 115–122.
Belega, B.A.: Bird-strike impact simulation with an aircraft wing using SPH bird model. INCAS Bulletin. Vol. 7 Issue 3, pp. 51–58, 2015.
Katukam, R.: Comprehensive bird strike simulation approach for aircraft structure certification. cyient white paper, 2014.
Chitte, P., Jadhav, P.K., Bansode, S.S.: Statistic and Dynamic Analysis of Typical Wing Structure of Aircraft using Nastran. IJAIEM Journal, Volume 2, Issue 7, July 2013.
Raj, N.S.N., Koti, H., Channankaiah: Static Stress Analysis for Aircraft Wing and Its Weight Reduction using Composite Material. International Journal of Engineering Research & Technology, Vol. 3 Issue 3, March – 2014, 2300–2303.
Huang, C.K., Lin K.Y.: A method for reliability assessment of aircraft structures subject to accidental damage. American Institute of Aeronautics and Astronautics Paper, pp. 1–10, 2005.
Prabhu, M.S., Raj J.N., Vignesh, G.: Optimization of Unmanned Aerial Vehicle Wing Structure. IJISET - International Journal of Innovative Science, Engineering & Technology, Vol. 2 Issue 3, March 2015, pp. 28–34.
Khan, H.N., Usama, M.W., Ahmad, R., Rasool, I.: 3-D CAD Modeling and Analysis of Aircraft Wing Using CATIA Software And Its Comparison With ANSYS Software. proceedings of the 4th international conference on Automation and Transportation Systems, Brasov, Romania, pp. 19–22, 2013.
Goud, T.S.K. Kumar A.S., Prasad, S.S.: Analysis of Fluid-Structure Interaction on an Aircraft Wing. International Journal of Engineering and Innovative Technology (IJEIT) Volume 3, Issue 9, March 2014, pp. 146–152.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2017 Springer Science+Business Media Singapore
About this paper
Cite this paper
Nitin Chandola, Rawat, R.S. (2017). Finite Element Analysis of Wing Design. In: Singh, R., Choudhury, S. (eds) Proceeding of International Conference on Intelligent Communication, Control and Devices . Advances in Intelligent Systems and Computing, vol 479. Springer, Singapore. https://doi.org/10.1007/978-981-10-1708-7_57
Download citation
DOI: https://doi.org/10.1007/978-981-10-1708-7_57
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-10-1707-0
Online ISBN: 978-981-10-1708-7
eBook Packages: EngineeringEngineering (R0)