Question

3.1 Find all of the external reactions for the externally braced monoplane wing with the air loads shown below Assume that: (i) the chordwise force of 6 lb./in. acts mainly on the rear spar, (ii) point B is designed so that it carries no reaction in the D-direction, (ii) the moment resistances at all connections are negligible, and (iv) the weight of the wing is negligible. Some Answers FCG = 4,740 lb (T) Ay 516.1 lb iuv By 258.2 lb u

Answer 1

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