SHIGLEY'S MECH.ENGIN....(LOOSE)>CUSTOM<
SHIGLEY'S MECH.ENGIN....(LOOSE)>CUSTOM<
10th Edition
ISBN: 9781260163155
Author: BUDYNAS
Publisher: MCG CUSTOM
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Chapter 9, Problem 30P
To determine

The bending force F.

Expert Solution & Answer
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Answer to Problem 30P

The bending force F is 1.77kip

Explanation of Solution

The below figure shows the dimension of the weld.

SHIGLEY'S MECH.ENGIN....(LOOSE)>CUSTOM<, Chapter 9, Problem 30P

Figure-(1)

Write the expression for throat area of weld-1.

A1=0.707hb1 . (I)

Here, the thickness of weld is h and length of weld is b1.

Write the expression for throat area of weld-2.

A2=0.707hb2 (II)

Here, the length of weld is b2.

Write the expression for throat area of weld-3.

A3=0.707hd (III)

Here, the length of weld is d.

Write the expression for total throat area.

A=A1+A2+A3 . (IV)

Write the expression for total length of the weld.

l=b1+b2+d (V)

Write the expression for location of centroid along x-direction.

X¯=x1b1+x2b2+x3b3l . (VI)

Here, the centroidal length of weld-1 is x1, the centriodal distance of length of weld-2 is x2 and the centriodal distance of weld-3 is x3.

Write the expression for centroid along y-direction.

Y¯=y1b1+y2b2+y3dl (VII)

Here, the centroidal distance of weld-1 is y1 , the centroidal distance of weld-2 is y2 and the centroidal distance of weld-3 is y3.

Write the expression for the length between total weld and weld-1.

r1=(b12X¯)2+(dY¯)2 (VIII)

Write the expression for length between total weld and weld-2.

r2=(b22X¯)2+(Y¯)2 . (IX)

Write the expression for length of total weld and weld-3.

r3=(X¯)2+(d2Y¯)2 . (X)

Write the expression for polar moment of inertia of weld-1 about its centroid.

J1=0.707hb1312 (XI)

Write the expression for moment of inertia of weld-2 about its centroid.

J2=0.707hb2312 (XII)

Write the expression for polar moment of inertia of weld-3 about its centroid.

J3=0.707hd312 . (XIII)

Write the expression for polar moment of inertia of the total weld.

J=(J1+A1r12)+(J2+A2r22)+(J3+A3r32) (XIV)

Write the expression for length where maximum secondary shear stress occurs.

r=Y¯2+(b2X¯)2 . (XV)

Write the expression for angle of r with x- axis.

α=tan1(Y¯b2X¯) (XVI)

Write the expression for moment about weld center.

M=F(c+b2X¯) (XVII)

Here, the load on the weld is F.

Write the expression for primary shear stress.

τ=FA . (XVIII)

Write the expression for secondary shear.

τ=MrJ (XIX)

Write the expression for maximum shear stress.

τmax=(τsinα)2+(τcosα+τ)2                                           (XX)

Conclusion:

Substitute 516in for h and 2in for b1 in Equation (I).

A1=0.707(516in)(2in)=0.707(0.625in2)=0.4418in2

Substitute 516in for h and 4in for b2 in Equation (II).

A2=0.707(516in)(4in)=0.707(1.25in2)=0.88375in2

Substitute 516in for h and 4in for d in Equation (II).

A3=0.707(516in)(4in)=0.707(1.25in2)=0.88375in2

Substitute 0.4418in2 for A1 , 0.88375in2 for A2 and 0.88375in2 for A3 in Equation (III).

A=0.4418in2+0.88375in2+0.88375in2=2.2093in2

Substitute 2in for b1 , 4in for b2 and 4in for d in Equation (IV).

l=2in+4in+4in=10in

Substitute 2in for b1 , 4in for b2 , 4in for d , 10in for l , 1in for x1 , 2in for x2 and 0in for x3 in Equation (V).

X¯=(1in)(2in)+(2in)(4in)+(0in×4in)10in=2in2+8in2+0in210in=10in210in=1in

Substitute 2in for b1 , 4in for b2 , 4in for d , 10in for l , 4in for y1 , 0in for y2 and 2in for y3 in Equation (V).

Y¯=(4in)(2in)+(0in)(4in)+(2in×4in)10in=8in2+0in2+8mm210in=16in210in=1.6in

Substitute 2in for b1 , 4in for d , 1in for X¯ and 1.6in for Y¯ in Equation (VI).

r1=(2in21in)2+(4in1.6in)2=(1in1in)2+(4in1.6in)2=0in2+5.76in2=2.4in

Substitute 4in for b2 , 1in for X¯ and 1.6in for Y¯ in Equation (VII).

r2=(4in21in)2+(1.6mm)2=(2in1in)2+(1.6in)2=2.56in2=1.6in

Substitute 4in for d , 1in for X¯ and 1.6in for Y¯ in Equation (VIII).

r3=(1in)2+(4in21.6in)2=(1in)2+(2in1.6in)2=1.16in2=1.077in

Substitute 516in for h and 2in for b1 in Equation (IX).

J1=0.707(516in)(2in)312=0.707(516in)(8in3)12=1.7675in412=0.1472in4

Substitute 516in for h and 4in for b2 in Equation (X).

J2=0.707(516in)(4in)312=0.707(516in)(64in3)12=14.14in412=1.178in4

Substitute 516in for h and 4in for d in Equation (XI).

J3=0.707(516in)(4in)312=0.707(516in)(64in3)12=14.14in412=1.178in4

Substitute 0.1472in4 for J1, 0.4418in2 for A1 , 0.88375in2 for A2 , 0.88375in2 for A3 , 1.178in4 for J2 , 1.178in4 for J3 , 2.4in for r1 , 1.6in for r2 and 1.077in for r3 in Equation (XII).

J=[(0.1472in4+(0.4418in2)(2.4in)2)+(1.178in4+0.88375in2(1.6in)2)+(1.178in4+(0.88375in2)(1.077in)2)]=[(0.1472in4+2.544in4)+(1.178in4+2.2624in4)+(1.178in4+1.0250in4)]=2.6912in4+3.4404in4+2.203in4=8.3346in4

Substitute 1.6in for Y¯ , 4in for b2 and 1in for X¯ in Equation (XIII).

r=(1.6in)2+(4in1in)2=2.56in2+(3in)2=11.56in2=3.4in

Substitute 1.6in for Y¯, 4in for b2 and 1in for X¯ in Equation (XIV).

α=tan1(1.6in4in1in)=tan1(1.6in3in)=tan1(0.533)=31.19°

Substitute 6in for c , 4in for b2 , Fkip for F and 1in for X¯ in Equation (XV).

M=(Fkip)(6in+4in1in)=(Fkip)(9in)=9Fkipin

Substitute Fkip for F and 2.2093in2 for A in Equation (XVI).

τ=Fkip2.2093in2=0.4526Fkip/in2

Substitute 9Fkipin for M , 3.4in for r and 8.3346in4 for J in Equation (XVII).

τ=(9Fkipin)(3.4in)8.3346in4=30.6Fkipin28.3346in4=3.67Fkip/in2

Substitute 3.67Fkip/in2 for τ , 31.19° for α , 25kpsi for τmax and 0.4526Fkip/in2 for τ in Equation (XVIII).

25kpsi={(3.67Fsin(31.19°)kip/in2)2+(3.67Fcos(31.19°)kip/in2+0.4526Fkip/in2)}225kpsi=(1.9006Fkip/in2)2+(3.136Fkip/in2+0.4526Fkip/in2)225kpsi=3.6122F2(kip/in2)2+12.8780F2(kip/in2)225kpsi=16.4902F2(kip/in2)2

25kpsi=14.0957FkpsiF=25kpsi14.0957FkpsiF=1.77kip

Thus, the bending force is 1.77kip

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Chapter 9 Solutions

SHIGLEY'S MECH.ENGIN....(LOOSE)>CUSTOM<

Ch. 9 - Prob. 11PCh. 9 - 99 to 912 The materials for the members being...Ch. 9 - 913 to 916 A steel bar of thickness h is welded to...Ch. 9 - 913 to 916 A steel bar of thickness h is welded to...Ch. 9 - 913 to 916 A steel bar of thickness h is welded to...Ch. 9 - Prob. 16PCh. 9 - Prob. 17PCh. 9 - 917 to 920 A steel bar of thickness h, to be used...Ch. 9 - 917 to 920 A steel bar of thickness h, to be used...Ch. 9 - 917 to 920 A steel bar of thickness h, to be used...Ch. 9 - Prob. 21PCh. 9 - 921 to 924 The figure shows a weldment just like...Ch. 9 - Prob. 23PCh. 9 - Prob. 24PCh. 9 - 9-25 to 9-28 The weldment shown in the figure is...Ch. 9 - 9-25 to 9-28 The weldment shown in the figure is...Ch. 9 - Prob. 27PCh. 9 - 925 to 928 The weldment shown in the figure is...Ch. 9 - The permissible shear stress for the weldment...Ch. 9 - Prob. 30PCh. 9 - 9-30 to 9-31 A steel bar of thickness h is...Ch. 9 - In the design of weldments in torsion it is...Ch. 9 - Prob. 33PCh. 9 - Prob. 34PCh. 9 - The attachment shown carries a static bending load...Ch. 9 - The attachment in Prob. 935 has not had its length...Ch. 9 - Prob. 37PCh. 9 - Prob. 39PCh. 9 - Prob. 40PCh. 9 - Prob. 42PCh. 9 - 9-43 to 9-45 A 2-in dia. steel bar is subjected to...Ch. 9 - 9-43 to 9-45 A 2-in dia. steel bar is subjected to...Ch. 9 - Prob. 45PCh. 9 - Prob. 46PCh. 9 - Find the maximum shear stress in the throat of the...Ch. 9 - The figure shows a welded steel bracket loaded by...Ch. 9 - Prob. 49PCh. 9 - Prob. 50PCh. 9 - Prob. 51PCh. 9 - Brackets, such as the one shown, are used in...Ch. 9 - For the sake of perspective it is always useful to...Ch. 9 - Hardware stores often sell plastic hooks that can...Ch. 9 - For a balanced double-lap joint cured at room...
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