NACA Wing RIB Design and Optimization
Authors
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M. S. Ramaiah Institute of Technology Bengaluru 560054, Affiliated to Visvesvaraya Technological University, Belgaum: MSRIT hostels (engg) Mathikere Bengaluru 560054 ,IN
Vasanth G. -
M. S. Ramaiah Institute of Technology Bengaluru 560054, Affiliated to Visvesvaraya Technological University, Belgaum: MSRIT hostels (engg) Mathikere Bengaluru 560054 ,INSunil Sunagad
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M. S. Ramaiah Institute of Technology Bengaluru 560054, Affiliated to Visvesvaraya Technological University, Belgaum: MSRIT hostels (engg) Mathikere Bengaluru 560054 ,INDarshan S. Mekali
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M. S. Ramaiah Institute of Technology Bengaluru 560054, Affiliated to Visvesvaraya Technological University, Belgaum: MSRIT hostels (engg) Mathikere Bengaluru 560054 ,INSiddlingesh A. U.
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M. S. Ramaiah Institute of Technology Bengaluru 560054, Affiliated to Visvesvaraya Technological University, Belgaum: MSRIT hostels (engg) Mathikere Bengaluru 560054 ,INVeeranna B. Nasi
DOI:
https://doi.org/10.18311/jmmf/2023/33350Keywords:
Design and optimization, different cut-out configurations, Experimentation cost, Changing dimensions, Wing RibAbstract
Design of wings and wing ribs are of paramount importance in the field of aircraft manufacturing. The wing ribs need to have high strength and needs to be as light weight as possible. To achieve this a compromise needs to be made on the strength of the wing rib. As cut-outs are made in wing ribs the weight is reduced, but the strength also decreases along with that. This paper will deal with the above-mentioned problem and try to reach an optimal ground of design to make cut-outs through which strength remains almost the same as the wing rib without cut-out but the overall weight is reduced. Optimization of the wing rib designs will be reached by using different materials and different cut-out configurations. The wing rib with the best overall features such as weight, strength and price from the combination of different materials and cut-outs will be found.
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References
Bairavi and Balaji, (2016): “Design and Stress Analysis of Aircraft Wing Rib with various cut outs” https:// www.worldwidejournals.com/indian-journal-of-appliedresearch (IJAR)/fileview/April_2016_1459503605
Bindu and Ali, (2013): “Design and Analysis of a Typical Wing Rib for passenger Aircraft”. https://1library.net/ document/zgxn5r2q-design-analysis-typical-wing-ribpassenger- aircraft.html
Kavya and Reddy, (2017): “Design and Finite Element Analysis of Aircraft Wing Using Ribs and Spars https:// 1library.net/document/zlnwv7lq- design-finite-elementanalysis- aircraft-using- guguloth-raghukumar.html
Sharma and Garg, (2014): “Design and Analysis of Wing Rib of Aircraft Review” https://1library.net/document/ z3n3lj9q-design-analysis-wing-rib-aircraft- review.html.
Bannaceur, Xu and Layachi, (2017): Wing Rib Stress Analysis and Design Optimization Using Constrained Natural Element.https://iopscience.iop.org/article/10.1088/ 1757-899X/234/1/012018/pdf.
Dharmendra,Chaitanya K J, Ayesha Sameera, Khyati Kavathiya, Monika K M “Design and Analysis of an Aircraft Wing Rib for Different Configurations”, International Journal of innovative Research in Science and Engineering, Vol. https://www.irjet.net/archives/V7/i6/ IRJE T-V7I635.pdf.
Ramin Sedaghati, Mostafa S.A. Elsayed, (2006): “Wing Rib Stress Analysis and Design Optimization. MOSAIC Project, CRIAQ 4.1-TASK 6.
