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Unformatted text preview: circle determine (a) the principal stresses (b) the maximum inplane shear stress and the average normal stress at the point. Draw the rotated element in each case. Problem 9.4 9.5 The internal loadings at a crosssection through the 6 in. diameter drive shaft of a turbine consist of an axial force of 2500 lb, a bending moment of 800 lbft, and a torsional moment of 1500 lbft. Determine the principal stresses at point B. Also compute the maximum inplane shear stress at this point....
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This homework help was uploaded on 04/18/2008 for the course EGRM 202 taught by Professor Speich during the Spring '07 term at VCU.
 Spring '07
 Speich

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