ae114
DESCRIPTION
Aerostructures IITRANSCRIPT
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AE114: Wednesday March 11, 2015
Exam 1 Review
Shear Center of an Open SectionThick Skin with no Stringers
Lab Problem 1 Assigned
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For a cantilever beam with a channel section, find a) the distribution of the resisting shear flow due to avertical downward force of V = 100 lb
b) the horizontal location of shear center
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First, find the shear flows beginning at a and working around to dIxNA of this section has been computed as:
IxNA = 0.2667 in4
To find the shear flow at station m, we integrate from a to m:
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There is an easier way to find the integral:
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Now we can find the location of the shear center.
First, convert the shear flows (lb/in) into concentrated forces (lb).This is done by finding the area (lb) from the shear flow diagram.
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