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The report analyzes the shear force and bending moment diagram of the CASA NC212 wing box, detailing the theory behind shear stress and bending moments, preliminary calculations, and load calculations. It employs the Schrenk method for lift distribution and provides specific calculations for wing dimensions, aerodynamic properties, and load distributions from lift, fuel, and engine weight. The findings confirm the accuracy of the shear force calculations, ensuring the model is reliable for further analysis.

Author

Tuấn Nguyễn Trịnh

Language

EN