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International Journal for Research in Applied Science & Engineering Technology (IJRASET)
from Optimization of Wing Rib Configurations for Improved Aerodynamic Performance A Computational Study
by IJRASET

ISSN: 2321-9653; IC Value: 45.98; SJ Impact Factor: 7.538
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Volume 11 Issue III Mar 2023- Available at www.ijraset.com
References
[1] Dharmendra P, Chaithanya K J, Ayesha Sameera, Khyati Kavathiya And Monika K M “ Design And Analysis Of An Aircraft Wing Rib For Different Configurations” International Research Journal of Engineering and Technology (IRJET) Volume: 07 Issue: 06 (June 2020)
[2] G. Lombardi and G. Mengali [2] An Optimization Procedure For The Conceptual Analysis Of Different Aerodynamic Configurations.
[3] Rahul Sharma and Garima Garg “Design and Analysis of Wing Rib of Aircraft Review” International Journal of innovative Research in Science and Engineering Technology, Vol. 3, Issue 12, (December 2014)
[4] Bindu H C, Muhammad Muhsin Ali H “Design and Analysis of a Typical Wing Rib for Passenger Aircraft” International Journal of innovative Research in Science and Engineering Technology, Vol. 2 Issue 7 (July 2013)
[5] Guguloth Kavya, 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, Issue No. 2348-4845