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Conjugate Beam METHOD

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Method (2)

Method (2)

 Conjugate beam Method ....

 Conjugate beam Method ....

Deflection (  Deflection ( yy)) )) Deflection (  Deflection ( yy))  Conjugate beam:  Conjugate beam: (Conjugate beam) (Conjugate beam) (Elastic load ) (Elastic load ) (  ( -M EI  EI  )-M ) ( M ) ( M )  Rotation or Slope( 

 Rotation or Slope( θθ)or (y')= )or (y')= Shear force Shear force of elastic of elastic load =load = Q Qelasticelastic

Deflection ( 

Deflection ( δ δ )or (y)= Moment of elastic load =)or (y)= Moment of elastic load = M Melasticelastic

 Real(Original) beam

 Real(Original) beam  Conjugate beam: Conjugate beam:

 Load =  Load =  d²M(x) d²M(x)dx²dx²  = w  = w  Shear = Shear =  dM(x) dM(x)dxdx  = = Q Q Moment = Moment = MM(x)(x)  Elastic load =

 Elastic load =  d²(y) d²(y)dx²dx²  =- =- EI  EI MM  Rotation =

 Rotation =  d(y) d(y)dxdx  = = Q Qelasticelastic

Deflection

Deflection = = y y == MMelasticelastic

wt/m' wt/m' Deflection) Deflection) Slope(  Slope( θθ)) Slope(  Slope( θθ     - M/EI  - M/EI   Rotation)  Rotation)

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θ

δ = 0 , θ ≠ 0 M = 0 , Q ≠ 0

Q

Free end Fixed support 

δ ≠ 0 , θ ≠ 0 M ≠ 0 , Q ≠ 0

Fixed support  Free end

δ = 0 , θ = 0

Q M

δ = 0 , θ ≠ 0 M = 0 , Q ≠ 0

Interior support (Roller or Hinge) Internal hinge

θL

θR

 (QL=QR ) Internal hinge

δ ≠ 0 , θL ≠ θR ≠ 0

Interior support (Roller or Hinge) θL θR

M ≠ 0 , QL ≠ QR

(Original beam)

(Conjugate beam)

M = 0 , Q = 0

End support (Roller or Hinge) End support (Roller or Hinge)

Conjugate Support 

 Real Support 

 Examples

 Real Beam Conjugate Beam

Indetreminate Beam

R = θL )

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Steps of Solution :

( y)

.Conjugate beam method 

 Reactions

 FOR Real beam

Bending Moment Diagram B.M.D)

 Examples 4 t/m` 2 t/m` 15 t  21 t  14 t  WL²/8=32m.t  WL²/8=9m.t  8 m.t  12 m.t  C 3t/m`

B.M.D

WL²  8 = 24m.t  6t  12t.m

=

WL²  8= 24m.t  12t.m (1) (2)

B.M.D

WL²/8=32m.t  WL²/8=9m.t  8 m.t  12 m.t 

B.M.D

6t   θ)

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4  (  (  C 12mt  8t  8t 

B.M.D

Modified B.M.D

12mt  6mt  12mt    12mt  12mt  24mt 

Or 

6mt  12mt  6mt  3mt  6mt 

 FOR Conjugate beam

(Conjugate Beam) (Conjugate Beam) (Elastic loads) .(Conjugate Beam) (C.g) .( B.M.D) .( B.M.D) ( B.M.D) ( Elastic loads) 1 2ML Datum ML Datum  nerti )  nerti ) (Elastic loads) (Given) .(Modified B.M.D) 8t  2 2   R  R

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2 3ML Datum Datum M1 M2 1 2M2L 1 2M1L Datum M1 M2 Datum M1 M2 = 1 2M1L 1 2M2L Datum M1 M2 = 2 3ML Datum Datum M1 M2 + 1 2M2L 1 2M1L Datum M1 M2 = + 2 3ML Datum Datum M1 M2 1 2M2L 1 2M1L

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(Deflection ) (Rotation)

 Rotation (  θ )= Deflection (y) =

Qelastic Melastic Q Q Q Q M M M M - v e  + v e +v e - v e  Positive )  Shear force Negtive )  Positive ) Moment  Negtive ) ( θ )= + ve  θ )= - ve y )= + ve y )= - ve Qelastic M elastic + -θ θ

Solved Examples

Using the Conjugate beam method, determine the rotation at points (a,b,c and d) and deflection at points(c,d and e).

 Ex(1)

 3t 

10t 10t  

 EI = Constant 

Solution

 Reactions and Bending moment diagram (Original beam)

 3t  10t 10t   16.2t  18.8t  10t 10t   2t/m' 2t/m' 6.0t.m 46.8t.m 47.4t.m  2*3² 8  =2.25 t.m  2*3² 8  =2.25 t.m a c d b e a c d b e 

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 Elastic loads( Area of bending moment)

6.0 46.8  47.4  2.25 t.m a c d b e 6.0 12 93.6 71.1  71.1  70.2 4.5  4.5 

Conjugate beam

a e a b e

 Elastic loads on Conjugate beam

a b e      6 .      0      1      2      9      3 .      6      7      1 .      1      7      0 .      2      7      1 .      1      4 .      5      4 .      5 a c d

 Elastic Reactions

a b e      6 .      0      1      2      9      3 .      6      7      1 .      1      7      0 .      2      7      1 .      1      4 .      5      4 .      5 a c d b 138.7  132.7  164.3   269.4 b

Modified B.M.D( M

 EI )

( M

 EI )

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 Required rotation and deflection

 Point (a)

 Rotation ( θ )= Qelastic Deflection (y) = Melastic

θa = 1EI[164.3] = + 164.3EI aa 164.3   Point (b) b 138.7  θb = 1EI[-138.7] = - 138.7EI  Point (c) θc = 1EI[164.3-4.5-71.1] = + 88.7EI      7      1 .      1      4 .      5 c 164.3  yc = 1EI[164.3(3)-4.5(1.5)-71.1(1)] = + 415.05 EI  Point (d) θd = 1EI[ -138.7 -12 +93.6] = - 57.1EI      1      2      9      3 .      6 d b      1      3      8 .      7  Point (e) e 132.7   269.4 θe = 1EI[ -132.7] = - 132.7EI ye = 1EI[ -268.8] = - 269.4EI  Left Right 

+ve Sign summary

+ ve   Clockwise   Anti-Clockwise   Clockwise   Down   Anti-Clockwise   Anti-Clockwise   Upward

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Using the Conjugate beam method, determine the rotation at points (a,b,c and d ) and deflection at points(c and d ).

 Ex(2)

4t  4t/m' I I 2I   b c a d

Solution

b c a d 4*6² 8  =18.0t.m 12t.m b c a d 12 6t.m 18t.m 9t.m 6  3  9  18  18  4.5  18   36  Elastic loads a d b       9 1     8      1      8      4 .      5      1      8      3       6  Elastic Reactions a d b       9 1     8      1      8      4 .      5      1      8      3       6 a 10.12 7.88  14.6 12.36

 Required rotation and deflection

 Point (a) θa = 1EI[+7.88] = + 7.88EI  Point (b) θb = 1EI[-14.62] = - 14.62EI  Point (c) yc = 1EI[14.62(3) + 4.5(1.0) -18(1.125)] = + 28.11EI θc = 1EI[18 - 14.62 - 4.5] = - 1.12EI c b      4 .      5      1      8 14.62 c  Point (d) yd = 1EI[+ 12.36] = + 12.36EI θd = 1EI[-10.12] = - 10.12EI

B.M.D

Conj.beam

I  I   2I 

I  I I    Clockwise   Anti-Clockwise   Downward   Anti-Clockwise   Downward   Anti-Clockwise

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 Ex(3)

Using the Conjugate beam method, determine :

* the rotation at points (a ,b,d and e ),

* the relative (change in) rotation at point( f ), * the deflection at points(d ,e ,f and j).

2t/m' 6t  a d b f  e c

Solution

 EI = Constant 

2t/m' 6t  a d b f  e c  3t  4t  a d b f  e c 9t.m 10t.m 16t.m 1t.m  5t.m 40 85.33  1.33   27  10 a d b e c  j 6.75t  16t  16.25t   j a d b f  e c 85.33  1.33   27  10 40 16  29.33   24.13  10.2 16  27  1.33  85.33  10 40

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11 

 Required rotations and deflections

 Point (a) θa = 1EI[+29.33] = + 29.33EI  Point (b) θb =1EI[-16] =-16EI a  29.33  b 16 θf/L = 1EI[-16+10-1.33] = - 7.33EI y = 1EI[-16(2)+10(1.33)-1.33(1)] = - 20EI

 Point (f)(Internal Hinge )

θf/R = 1EI[-16+10-1.33+24.13 ] = + 16.8EI θf/rel = [θf/R - θf/L ]= + 16.8EI - -7.33EI  = + 24.13EI  = Rf EI f        1  .       3       3       1        0 16  24.13   Point (d) yd=1EI[+29.33(4)+10(1.33)-42.7(1.5)] =+66.6EI a d 16t.m  5t.m 42.7  10  29.33   Point (e) ye=1EI[+10.2(3)-13.5(1)] = + 17.1EI e c 9t.m 13.5  10.2  Point (j) M  j= 6.75(3) - 6(1.5) = 11.25t.m 2t/m' a 6.75t   j 11.25t.m  29.33 

 Real beam Conj. beam

 2.25 t.m 16.88  4.5  y  j = 1EI[+29.33(3)-16.88(1) -4.5(1.5)] = + 64.36 EI θd = 1EI θe = 1EI   Clockwise)   Anti-Clockwise)   Anti-Clockwise)   Upward)   Clockwise)   Downward)   Downward)   Downward) [29.33+10-42.7] = - 3.37EI [13.5-10.2 ] = + 3.3EI 6t    Anti-Clockwise)   Clockwise)

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Using the Conjugate beam method, determine : * the rotation at points (c and e ),

* the relative (change in) rotation at point( d ),

* the deflection at points(c ,e and d ). [take EI = 6000 t/cm²]

 Ex(4)

 2I   2I  I  I  4t  a d e b c 2t/m'

Solution

 Reactions(Original beam)  2I   2I  I  I  4t  a d e b c 2t/m' 7t  13t  7t  a d e b c 7t.m 4t.m 8t.m 16t.m

B.M.D(Original beam)

a d e b c 7t.m 4t.m 4t.m 16t.m  2t.m  3.5  8.0 4.0 8.0 4.0 42.67   21.33  Conjugate beam  Elastic Reactions 16.29  a d e c 8.0 4.0 8.0 4.0  21.33   3.5  42.67   24.2 12.29   27.25  16t  7.0t.m

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 Required rotations and deflections

 Point (c) c 12.29   27.25  θc = 6000[-12.29] = - 0.002rad1 θd/L = 6000[+ 3.5] = 5.833*101 -4 rad yd = 6000[3.5(0.67)] = + 0.039 cm1 yc = 6000[-27.25] = - 0.454 cm1

 Point (d)(Internal Hinge ) a d

      3  .       5  24.2 θd/R = 6000[+ 3.5 + 24.2 ] = + 4.6167*101 -3 θd/rel = θd/R - θd/L= RdEI  = 6000  = 4.033*1024.2 -3 rad  Point (e) θe = 6000[-16.29-8-4+21.33] = - 0.00116 rad1 ye = 6000[16.29*4 + 8*2.67+ 4*1.33-21.33*1.5] = + 0.997 cm1 16.29  e 4.0 8.0  21.33    Anti-Clockwise   Clockwise   Downward   Upward  Clockwise   Anti-Clockwise   Downward

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References

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