Problem 2.13. Curved beam

 A rectangular curved beam is subjected to uniform bending moment, M. Height, d and width, h of the cross section are given. Determine and sketch stresses σφ and σr , if

r¯d=2, 5,10

where

a) d = 0.4 m, h = 0.2 m, M = 120 kNm,

b) d = 0.3 m, h = 0.2 m, M = 100 kNm,

c) d = 0.4 m, h = 0.15 m, M = 140 kNm.

Solve Problem

Solve

Check the results for the first set of initial data. 

Problem a)

r¯d=2

σφ(r=ri) N/mm2 =×106

σφ(r=ro) N/mm2 =×106

σr(r=r¯) N/mm2 =×106

Sketch stresses.

Compare figure


See Figure 2.33.

  

Calculate all the other results and compare them to the Table hided below.

Check table

Problem a)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 2.706×107 2.411×107 2.328×107
σφ(r=ri) [N/mm2] -1.93×107 -2.11×107 -2.178×107
σr(r=r¯) [N/mm2] 2.792×106 1.124×106 5.623×105

 

Problem b)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 4.01×107 3.572×107 3.448×107
σφ(r=ri) [N/mm2] -2.86×107 -3.126×107 -3.226×107
σr(r=r¯) [N/mm2] 4.136×106 1.664×106 8.331×105

 

Problem c)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 4.21×107 3.751×107 3.621×107
σφ(r=ri) [N/mm2] -3.003×107 -3.282×107 -3.387×107
σr(r=r¯) [N/mm2] 4.343×106 1.748×106 8.748×105

 

 

Do you need help?

Steps

Step by step

Solution for the first set of initial data of Problem a) is presented.

Step 1. Express the radii of the curvature at the edges of the beam from the initial data.

Check curvatures

d= 0.4 m, r¯d=2      r¯=0.8 mro=r¯+d2= 1 mri=r¯d2= 0.6 m

Step 2. Calculate axial stresses, σφ at the edges of the cross section.

Check axial stress

Formulas for the calculation are given in  Figure 2.33.

R=(ro2ri2)24×ro2ri2lnrori2=0.0338 m4σφ=4MRhro2ri2ro2ri2r2lnrori+ro2lnrrori2lnrriAt internal edgeσφ(r=ri)=4MRhro2ri2ro2lnrori+ro2lnriro=2.706×104kNm2=27.06Nmm2At external edgeσφ(r=ro)=4MRhro2ri2ri2lnroriri2lnrori=1.93×104kNm2=19.30Nmm2

Step 3. Calculate radial stresses, σr at the middle of the cross section.

Check radial stress

Formulas for the calculation are given in  Figure 2.33.

R=(ro2ri2)24×ro2ri2lnrori2=0.0338 m4σr=4MRhro2ri2r2lnrori+ro2lnrror2lnrriAt the middle of the cross sectionσφ(r=r¯)=4MRhro2ri2r2lnrori+ro2lnr¯ror2lnr¯ri=2.791×103kNm2=27.91Nmm2

See Figure 2.33.

Step 4. Sketch stresses.

Compare figure

Step 5. Calculate all the other results and compare them to the Table hided below.

Check table

Problem a)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 27.06 24.11 23.28
σφ(r=ri) [N/mm2] -19.30 -21.10 -21.78
σr(r=r¯) [N/mm2] 2.792 1.124 0.5623

 

Problem b)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 40.10 35.72 34.48
σφ(r=ri) [N/mm2] -28.6 -31.26 -32.26
σr(r=r¯) [N/mm2] 4.136 1.664 0.833

 

Problem c)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 42.10 37.51 36.21
σφ(r=ri) [N/mm2] -30.03 -32.82 -33.87
σr(r=r¯) [N/mm2] 4.343 1.748 0.875

Results

Worked out solution

Solution for the first set of initial data of Problem a) is presented.

The radii of the curvature at the edges of the beam are expressed from the initial data:

d= 0.4 m, r¯d=2      r¯=0.8 mro=r¯+d2= 1 mri=r¯d2= 0.6 m

Axial stresses, σφ at the edges of the cross section are

σφ=4MRhro2ri2ro2ri2r2lnrori+ro2lnrrori2lnrri, whereR=(ro2ri2)24×ro2ri2lnrori2=0.0338 m4At internal edgeσφ(r=ri)=4MRhro2ri2ro2lnrori+ro2lnriro=27.06Nmm2At external edgeσφ(r=ro)=4MRhro2ri2ri2lnroriri2lnrori=19.30Nmm2

Radial stresses, σr are

σr=4MRhro2ri2r2lnrori+ro2lnrror2lnrri, whereR=(ro2ri2)24×ro2ri2lnrori2=0.0338 m4At the middle of the cross sectionσφ(r=r¯)=4MRhro2ri2r2lnrori+ro2lnr¯ror2lnr¯ri=2.791Nmm2

See Figure 2.33.

All the other results are given in the Table below.

Problem a)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 27.06 24.11 23.28
σφ(r=ri) [N/mm2] -19.30 -21.10 -21.78
σr(r=r¯) [N/mm2] 2.792 1.124 0.562

 

Problem b)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 40.10 35.72 34.48
σφ(r=ri) [N/mm2] -28.60 -31.26 -32.26
σr(r=r¯) [N/mm2] 4.136 1.664 0.833

 

 

Problem c)  r¯d=2 r¯d=5 r¯d=10
σφ(r=ro) [N/mm2] 42.10 37.51 36.21
σφ(r=ri) [N/mm2] -30.03 -32.82 -33.87
σr(r=r¯) [N/mm2] 4.343 1.748 0.875