HW8 - 3. Find the shear flow for the three-stringer section...

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EAS4200C Aerospace Structures Homework #8 (Due: Nov. 6th) 1 Find the flexural shear flow produced by the transverse shear force V z = 1,000N in the beam with the thin-walled section given in the figure. Sketch the shear flow on the cross-section. Assume that V z is applied at the shear center. 2. Find the shear center of the cross-section above.
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Unformatted text preview: 3. Find the shear flow for the three-stringer section shown in the figure for V z = 5,000N and V y = 0. Given shear modulus G = 27GPa, find the twist angle per unit length. Also determine the shear center. Is the shear flow statically determinate?...
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This note was uploaded on 06/06/2011 for the course EAS 4200C taught by Professor Kim during the Spring '09 term at University of Florida.

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