Vol. 5 No. 7 (2019) · Articles
Antony Samuel Prabu G
Department of Aeronautical Engineering & MVJCE, IN
N Vara Prasanth
Department of Aeronautical Engineering & MVJCE, IN
Aasish T
Department of Aeronautical Engineering & MVJCE, IN
B Vinay
Department of Aeronautical Engineering & MVJCE, IN
Channamallikarjun
Department of Aeronautical Engineering & MVJCE, IN
Keywords: CFRP-carbon reinforced polymer, Ribs, Spar, Cruise load, axial loads.
The ribs gives the proper aerodynamic shape to the wing. And spar will take most of the bending loads in wing structure. In the present work ribs, spars and wing structure is optimized for twisting, bending and axial loads in terms of size and shape for a particular 10 seater aircraft. CFRP is considered for the material configuration of the wing. Cruise load is considered for the analysis of the wing. Design has been made using Catia V5 R21 and Analysis has been carried out using ANSYS 14.5 workbench. The results are validated using standard design of the 10 seater Cessna 402 aircraft.
NA
Antony Samuel Prabu G, N Vara Prasanth, Aasish T, B Vinay, Channamallikarjun, “STRUCTURAL DESIGN & OPTIMIZATION OF AIRCRAFT WING SPAR,” International Journal of Technical Innovation in Modern Engineering & Science, vol. 5, no. 7, pp. 344-350, Jul 2019.
Copyright (c) 2019 Antony Samuel Prabu G, N Vara Prasanth, Aasish T, B Vinay, Channamallikarjun
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
Submission of a manuscript implies that the work described has not been published before, that it is not under consideration for publication elsewhere, and that if accepted, the author retains copyright with no restrictions. Authors may post the final peer-reviewed manuscript (postprint) to any repository or website.
