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Page 287
V Homework Problems 6.13 Refer to the cantilever beam depicted in Figure H6.
13 with an origin at A. Substitute the given loading intensity function w(x) into Eq.
6. 12 and perform the necessary integrations required to express shear, moment,
...
V Homework Problems 6.13 Refer to the cantilever beam depicted in Figure H6.
13 with an origin at A. Substitute the given loading intensity function w(x) into Eq.
6. 12 and perform the necessary integrations required to express shear, moment,
...
Page 288
For an origin at point A, substitute the loading function w(x) into Eq. 6.12 and
derive equations for shear, moment, slope, and deflection as functions of x.
Sketch these functions and check to see that all boundary conditions are satisfied
. 77777/.
For an origin at point A, substitute the loading function w(x) into Eq. 6.12 and
derive equations for shear, moment, slope, and deflection as functions of x.
Sketch these functions and check to see that all boundary conditions are satisfied
. 77777/.
Page 289
6.22 With an origin at the right end of the cantilever depicted in Figure H6.22, the
loading varies as the cube of x/L to a maximum intensity of w,, when x = L.
Substitute this given loading intensity function w(x) into Eq. 6. 12 and perform the
...
6.22 With an origin at the right end of the cantilever depicted in Figure H6.22, the
loading varies as the cube of x/L to a maximum intensity of w,, when x = L.
Substitute this given loading intensity function w(x) into Eq. 6. 12 and perform the
...
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Contents
Internal Forces in Members | 1 |
Hollow Circular ShaftsAngle of Twist and Shearing Stresses | 157 |
4i5 Power Transmission | 169 |
Copyright | |
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absolute maximum shear allowable stress aluminum angle of twist applied Assume axial force axially loaded beam shown bending cantilever beam Castigliano's second theorem circular column components compressive Compute constant construct coordinate cross section cross-sectional area cylinder deflection deformation depicted in Figure Determine diameter differential elastic curve equal equation equilibrium factor of safety flexural stress free-body diagram function given by Eq Homework Problems k-ft k-in kN-m length longitudinal material maximum shear stress modulus of elasticity Mohr's circle neutral axis normal stress obtained perpendicular plane stress plot principal centroidal axis principal stresses radius Refer to Figure respect rotation section a-a segment shear center shear force shear strain shown in Figure slope Solution Solve static statically indeterminate steel stress element subjected Substitution tension tion torque torsional uniform load vertical yield strength yield stress zero