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Question # 5 In the early design the aircraft wing is consider as a spar. In the design, the wing semi- spar is 5m, and is assumed to carry a uniformly

distributed lifting load of 5000 N/m during stead level ↑↑↑↑↑↑↑ 5m ↑↑↑↑↑↑↑↑

Fig: 1