A Review on Design Optimization of an Aircraft Wing with Emphasis on Vibration Characteristics
Citation
Nataraj Kuntoji, Dr. Vinay V. Kuppast "A Review on Design Optimization of an Aircraft Wing with Emphasis on Vibration Characteristics", International Journal of Engineering Trends and Technology (IJETT), V48(3),147-151 June 2017. ISSN:2231-5381. www.ijettjournal.org. published by seventh sense research group
Abstract
It is essential that the structural stability of the aircraft wings is a major consideration in the design of the aircraft. Many studies are being carried out for the design of the wings across the globe by the researches to strengthen the aircraft wings for steady and sturdy structures for dynamic conditions.
The design of the aircraft wing using NACA standards is been discussed in this review. The wing analysis is carried out by using computer numerical analysis tool, viz., CAD/CAE and CFD. The optimization of the aircraft wing is effectively achieved by considering different material properties, loading conditions and dimensions with different flying conditions. The modal analysis is considered to analyse the wing to determine the natural frequency for vibration characteristics of the wing structure. The proposed work is identified in carrying out the wing analysis for vibration characteristics using computational tools, and then a prototype of wing structure. The validation of the prototype can be done by experimental method for the optimized wing design.
References
[1] ATSB Transport Safety Report [Insert Mode] Occurrence Investigation, AO-2013-226, Final -21 January 2016, Australian Transport Safety Bureau.
[2] E.N. Jacobs, K.E. Ward, & R.M. Pinkerton. NACA Report No. 460, "The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel". NACA, 1933.
[3] Nguyen Minh Triet, Nguyen Ngoc Viet, and Pham Manh Thang “Aerodynamic Analysis of Aircraft Wing” VNU Journal of Science: Mathematics – Physics, Vol. 31, No. 2 (2015) 68-75.
[4] Kakumani Sureka and R Satya Meher “Modeling and Structural Analysis on A300 Flight Wing by using ANSYS” International Journal of Mechanical Engineering and Robotics Research Vol. 4, No. 2, April 2015.
[5] Sudhir Reddy Konayapalli and Y Sujatha “Design and Analysis of Aircraft Wing” International Journal and Magazine of Engineering, Technology, Management and Research. Volume No: 2 (2015), Issue No: 9 (September).
[6] S. Senthilkumar, A. Velayudham, and P. Maniarasan “Dynamic Structural Response Of An Aircraft Wing Using Ansys” International Journal of Engineering Research & Technology (IJERT), Vol. 2 Issue 6, June – 2013.
[7] Lica Flore and Albert Arnau Cubillo “ Dynamic Mechanical Analysis of an Aircraft Wing with emphasis on vibration modes change with loading” International Conference of Scientific Paper AFASES 2015 Brasov, 28-30 May 2015.
[8] Guguloth Kavya and B.C Raghukumar Reddy “Design and Finite Element Analysis of Aircraft Wing using Ribs and Spars” International Journal and Magazine of Engineering, Technology, Management and Research. Volume No: 2 (2015), Issue No: 11 (November).
[9] T.S.Vinoth Kumar, A.Waseem Basha, M.Pavithra, and V.Srilekha “Static and Dynamic Analysis of a Typical Aircraft Wing Structure using MSC Nastran” International Journal of Research in Aeronautical and Mechanical Engineering, Volume: 3 Issue 8, August 2008.
[10] Farrukh Mazhar and Abdul Munem Khan “ Structural Design of a UAV Wing using Finite Element Method” 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
18th 12 - 15 April 2010, Orlando, Florida.
[11] Beulah Saripalli, Ratnakar Pandu, and Vijay John “Vibration and CFD Analysis of Hybrid Composite Wing” International Journal of Novel Research in Electrical and Mechanical Engineering Vol. 2, Issue 3, pp: (105-116), Month: September-December 2015.
Keywords
Aircraft Wing structure, Stress analysis, Modal analysis, CATIA V5R19, CFD.