A wing spar is a crucial structural component of an aircraft's wing, providing essential support and...

  

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A wing spar is a crucial structural component of an aircraft's wing, providing essential support and strength. As the primary load-bearing member, it is designed to withstand transverse shear loads and spanwise bending. Consider a 10 m aircraft wing, as shown below. You are required to design three types of spar structures: C-channel section Box beam section l-beam section Calculate the maximum shear stress and bending moment of the given wing spar for each beam design. Evaluate each design by providing justifications and insightful comments on the results. Based on the calculations and analysis, recommend the most suitable spar. Note: You can propose beam section dimensions based on the given geometry of the wing. 20 cm (height) 80 cm (chord length) 3m 200 kg 5 kN/m 7m 10 m (wing span) A wing spar is a crucial structural component of an aircraft's wing, providing essential support and strength. As the primary load-bearing member, it is designed to withstand transverse shear loads and spanwise bending. Consider a 10 m aircraft wing, as shown below. You are required to design three types of spar structures: C-channel section Box beam section l-beam section Calculate the maximum shear stress and bending moment of the given wing spar for each beam design. Evaluate each design by providing justifications and insightful comments on the results. Based on the calculations and analysis, recommend the most suitable spar. Note: You can propose beam section dimensions based on the given geometry of the wing. 20 cm (height) 80 cm (chord length) 3m 200 kg 5 kN/m 7m 10 m (wing span)