Enhanced Wing Efficiency Via Differential Thermal Coefficient Of Expansion Spar Caps SMITH; CHARLES R. [NORTHROP GRUMMAN SYSTEMS CORPORATION]
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SOLVED: What is the average stress in the spar cap of the following wing with the given loading? Assume all bending is taken by the spar caps, each cap with the given
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22.16.2. Main Wing Box - Abbott Aerospace UK Ltd
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