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Timothy A. Philpot - Mechanics of materials _ an integrated learning system-John Wiley (2017)

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15.3 principal Stresses in a Flexural member

Procedures for locating the critical sections of a beam (i.e., the maximum internal shear

force V and the maximum bending moment M) were presented in Chapter 7. Methods

for calculating the bending stress at any point in a beam were presented in Sections 8.3

and 8.4. Methods for determining the horizontal and transverse shear stresses at any

point in a beam were presented in Sections 9.5 through 9.7. However, the discussion of

stresses in beams is incomplete without a consideration of the principal and maximum

shear stresses that occur at the locations of maximum shear force and maximum bending

moment.

The normal stress caused by flexure is largest on either the top or bottom surfaces of

a beam, but the horizontal and transverse shear stress is zero at these locations. Consequently,

the tensile and compressive normal stresses on the top and bottom surfaces of

the beam are also principal stresses, and the corresponding maximum shear stress is

equal to one-half of the bending stress [i.e., τ max = (s p − 0)/2]. On the neutral surface, the

normal stress due to bending is zero; however, the largest horizontal and transverse shear

stresses usually occur at the neutral surface. In this instance, the principal and maximum

shear stresses are both equal to the horizontal shear stress. At points between these

extremes, one might well wonder whether there are combinations of normal and shear

stresses that create principal stresses larger than those at the extremes. Unfortunately, the

magnitude of the principal stresses throughout a cross section cannot be expressed as a

simple function of position for all sections; however, contemporary analytical software

often provides insight into the distribution of principal stresses by means of color-coded

stress contour plots.

Rectangular cross Sections

For beams with a rectangular cross section, the largest principal stress is usually the maximum

bending stress, which occurs on the top and bottom surfaces of the beam. The maximum

shear stress usually occurs at the same location and has a magnitude equal to one-half

of the bending stress. Although it may be of lesser intensity, the horizontal shear stress

(calculated from τ = VQ/It) at the neutral surface may also be a significant factor, particularly

for materials having a horizontal plane of weakness, such as a typical timber beam.

Flanged cross Sections

If the beam cross section is a flanged shape, then principal stresses at the junction between

flange and web must also be investigated. When a beam with a flanged cross section is

subjected to a combination of large V and large M, the bending and transverse shear stresses

that occur at the junction of the flange and the web sometimes produce principal stresses

that are greater than the maximum bending stress at the outermost surface of the flange. In

general, at any point in a beam, a combination of large V, M, Q, and y, together with a small

t, should suggest a check of the principal stresses at such a point. Otherwise, the maximum

bending stress will very likely be the principal stress, and the maximum in-plane shear

stress, will probably occur at the same point.

Stress Trajectories

Knowledge of the directions of the principal stresses also may aid in the prediction of

the direction of cracks in a brittle material (e.g., concrete) and thus may also aid in the

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