A Review on Design Optimization of an Aircraft Wing with Emphasis on Vibration Characteristics
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International Journal of Engineering Trends and Technology (IJETT) | 
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| © 2017 by IJETT Journal | ||
| Volume-48 Number-3 |
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| Year of Publication : 2017 | ||
| Authors : Nataraj Kuntoji, Dr. Vinay V. Kuppast |
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| DOI : 10.14445/22315381/IJETT-V48P226 |
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
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Keywords
Aircraft Wing structure, Stress analysis, Modal analysis, CATIA V5R19, CFD.