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FEA of CFRP Aircraft Wing Rib Integrity by Prasanna Kumar T.J. is a document available to read on EtoBox.
This study employs Finite Element Analysis (FEA) to evaluate the structural behavior of an aircraft wing rib under aerodynamic and mechanical loads, using ANSYS 13.0 for modeling. The analysis identifies critical stress zones and deformation patterns, highlighting areas for design optimization to enhance structural integrity and weight efficiency. Results indicate that while the rib can withstand operational stresses, localized reinforcements may be necessary near high-stress regions, particularly around cu
- Author
- Prasanna Kumar T.J.
- Language
- EN