Question: 2 . For the aircraft wing shown below, a . Calculate the resultant vertical force at the wing root, and the resultant moment. b .

2. For the aircraft wing shown below,
a. Calculate the resultant vertical force at the wing root, and the resultant moment.
b. Repeat this with the addition of a 300 kg wing tank located 2.6 m from the wing root.
2 . For the aircraft wing shown below, a .

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