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MECHANICS OF MATERIALS

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Presentation on theme: "MECHANICS OF MATERIALS"— Presentation transcript:

1 MECHANICS OF MATERIALS
Third Edition MECHANICS OF MATERIALS CHAPTER Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University Shearing Stresses in Beams and Thin- Walled Members © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

2 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Introduction Transverse loading applied to a beam results in normal and shearing stresses in transverse sections. When shearing stresses are exerted on the vertical faces of an element, equal stresses must be exerted on the horizontal faces Longitudinal shearing stresses must exist in any member subjected to transverse loading. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

3 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Shear on the Horizontal Face of a Beam Element shear flow=q= 𝑉𝑄 𝐼 Q= the horizontal force per unit length or shear flow Q is the first moment with respect to the neutral axis of the portion of the cross section located either above or below the point at which q is being computed, and that I is the centroidal moment of inertia of the entire cross-sectional area. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

4 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Example 6.01 SOLUTION: Determine the horizontal force per unit length or shear flow q on the lower surface of the upper plank. Calculate the corresponding shear force in each nail. A beam is made of three planks, nailed together. Knowing that the spacing between nails is 25 mm and that the vertical shear in the beam is V = 500 N, determine the shear force in each nail. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

5 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Example 6.01 SOLUTION: Determine the horizontal force per unit length or shear flow q on the lower surface of the upper plank. VQ (500N)(120 ×10−6 m3) 16.20 ×10-6 m4 m Calculate the corresponding shear force in each nail for a nail spacing of 25 mm. F = (0.025 m)q = (0.025 m)(3704 N m q = = I Q = Ay = (0.020 m × m)(0.060 m) = 120 ×10−6 m3 = 3704 N I = 1 (0.020 m)(0.100 m)3 12 + 2[ 1 (0.100 m)(0.020 m)3 12 + (0.020 m × m)(0.060 m)2 ] = ×10−6 m4 F = 92.6 N © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

6 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Determination of the Shearing Stress in a Beam The average shearing stress on the horizontal face of the element is obtained by dividing the shearing force on the element by the area of the face. = VQ It On the upper and lower surfaces of the beam, τyx= 0. It follows that τxy= 0 on the upper and lower edges of the transverse sections. τ ave © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

7 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Shearing Stresses τxy in Common Types of Beams For a narrow rectangular beam, 3 V τ max = 2 A For American Standard (S-beam) and wide-flange (W-beam) beams VQ τ ave = It V τ = max Aweb © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

8 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Sample Problem 6.2 SOLUTION: Develop shear and bending moment diagrams. Identify the maximums. Determine the beam depth based on allowable normal stress. Determine the beam depth based on allowable shear stress. Required beam depth is equal to the larger of the two depths found. A timber beam is to support the three concentrated loads shown. Knowing that for the grade of timber used, σ all = 1800 psi τ all = 120 psi determine the minimum required depth d of the beam. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

9 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Sample Problem 6.2 SOLUTION: Develop shear and bending moment diagrams. Identify the maximums. Vmax = 3kips M max = 7.5 kip ⋅ ft = 90 kip ⋅ in © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

10 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Sample Problem 6.2 Determine the beam depth based on allowable normal stress. = M max σ all S 3 1800 psi = 90 ×10 lb ⋅ in. (0.5833in.)d 2 d = 9.26in. Determine the beam depth based on allowable shear stress. I = 1 b d 3 12 S = I = 1 b d 2 c 6 = 3 Vmax τ all 2 A = 1 (3.5in.)d 2 6 = (0.5833in.)d 2 120 psi = lb 2 (3.5in.)d d = 10.71in. Required beam depth is equal to the larger of the two. d = 10.71in. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

11 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Sample Problem 6.3 SOLUTION: For the shaded area, Q = (4.31in)(0.770in)(4.815in) = 15.98in3 The shear stress at a, VQ (50 kips)(15.98in3 ) Knowing that the vertical shear is 50 kips in a W10x68 rolled-steel beam, determine the horizontal shearing stress in the top flange at the point a. τ = = (394in4 )(0.770in) It τ = 2.63ksi © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

12 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Unsymmetric Loading of Thin-Walled Members Beam loaded in a vertical plane of symmetry deforms in the symmetry plane without twisting. My VQ σ x = − τ ave = I It Beam without a vertical plane of symmetry bends and twists under loading. My VQ σ x = − τ ave ≠ I It © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

13 MECHANICS OF MATERIALS
Edition Third Beer • Johnston • DeWolf Unsymmetric Loading of Thin-Walled Members If the shear load is applied such that the beam does not twist, then the shear stress distribution satisfies = VQ D B E F = q ds = − q ds = −F′ τ V = q ds B A D ave It F and F’ indicate a couple Fh and the need for the application of a torque as well as the shear load. F h = Ve When the force P is applied at a distance e to the left of the web centerline, the member bends in a vertical plane without twisting. © 2002 The McGraw-Hill Companies, Inc. All rights reserved.

14 Determine the shear stress distribution for
Edition Third MECHANICS OF MATERIALS Beer • Johnston • DeWolf Example 6.06 Determine the shear stress distribution for V = 2.5 kips. τ = q = VQ t It © 2002 The McGraw-Hill Companies, Inc. All rights reserved.


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