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Theory of Structures(1) Lecture No. 1
[object Object],[object Object],[object Object],[object Object],[object Object],Chapter 1 : Loads and Reactions
Chapter 2  : Statically Determinate Beams   ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],A Beam :  is a structural member subjected to some external forces.
Chapter 3 :  Statically Determinate Rigid Frames ,[object Object],[object Object],A Frame : is a structure composed of a  number of members  connected together by joints all or  some are rigid.
Chapter 4 :  Statically Determinate Arches ,[object Object],[object Object],[object Object],[object Object],An Arch  :is a curved beam or two curved beams connected  together  by intermediate hinge.
Chapter 5 :  Statically Determinate Trusses ,[object Object],[object Object],[object Object],A truss :  Consists of  a number of straight members pin-  connected together and subjected to concentrated loads at  hinges.
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Roller Hinged Fixed Link
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Y B X A Y A Solution of Example 1 1- ∑ X  = 0   XA – 5 = 0   XA = 5t 2- ∑MB = 0   YA × 6 – 2 × 6 × 3 + (4 × 3)/2 × 1 = 0  YA= 5t 3- ∑ Y  = 0    YA + YB = 2 × 6+ (4 × 3)/2=18   YB = 13t
Solution of Example 2 1-       ∑ X  = 0   X A  = 3t 2-       ∑ M B  = 0 Y A × 4 + 8 + 4 × 1 – 3 × 1= 0  Y A = -2.25t ↑ Y A =2.25t ↓ 3-  ∑ y = 0   Y A  + 2× 2 = Y B   2.25+ 4 = Y B   Y B  = 6.25 t ↑ Y A X A Y B
Solution of Example 3 1- ∑ X = 0  XB – 4 = 0  XB = 4t 2- ∑ MA = 0 10YB – 4 × 12 – 2 × 9 – 2 × 5× 2.5 – 4 × 3= 0 YB = 10.3 t 3- ∑ Y = 0 YA + YB = 4 + 2 + 10 = 16   YA = 5.7 t Y B Y A X B
Solution of Example 4 1- ∑ X = 0 XA – 4 = 0  XA = 4t 2- ∑ Y = 0  YA – 1 × 6 – 5 – 5 – 2.5 = 0  YA = 18.5 t 3- ∑ M / A = 0 MA – 5 × 2 – 5 × 4 – 2.5 ×6 - 1×6×3 = 0   M A  = 63 t.m
Solution of Example 5 R 1  =  1/2 × 4 × 8 = 16 t R 2  = 0.5 × 4 = 2 t 1- ∑ X =  0  X A  – R 2  = 0 X A  = 2t  2- ∑ M A = 0  11 Y B  + 2 × 13 – R 2  × 2 – 2 × 1 – R 1  × 7= 0 Y B  = 8.36 t 3- ∑ Y = 0  Y A + Y B + 2 – 2 – 16 = 0 YA= 7.64t
Solution of Example 6 1- ∑ X = 0  X B  – 20 = 0   X B  = 20t 2- ∑ M A  = 0  6 Y B  + 20 × 3 – 10 × 6 – 20 × 6 = 0    Y B  = 20t 3- ∑Y = 0  Y A  + Y B  = 20 + 30 + 10 = 60    Y A  = 40t
Solution of Example 7 ∑  MO = 0 3 × 0 + 8 × 1 + 1 × 3 – Rd × 5 = 0 Rd = 2.2 t ↑ ∑  Mp = 0 1 × 2 + 8 × 4 + 3 × 5 – Rb × 5  = 0 Rb = 6.93t  ∑  Mq = 0 1 × 2 + 8 × 4 + 3 × 5 – Rc × 5  = 0 Rc = 6.93t 8t
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Solution of Example 8 Method I 1- Part FD   1) ∑ MD = 0  8 × 2 = 4 YF   YF = 4t 2) ∑Y = 0 YD = 8 – 4    YD = 4t 2- Part ECF 1) ∑ ME = 0 10×2.5+4×5= 4YC  YC= 11.25t 2) ∑Y = 0    YE=10+4-11.25  YE=2.75t 3- Part ABE 1) ∑MA=0 12×3+2.75×6=5YB   YB=10.5t 2) ∑Y = 0   YA= 2.75 + 12-10.5   YA= 4.25t
Solution of Example 8 “ Continued ” Method II 1)∑MF(right)= 0 8 × 2 – 4 YD = 0 YD = 4t 2) ∑ME(right)= 0 18×4.5 – 4×9 – 4YC= 0 YC=11.25t 3) ∑MA = 0 30×7.5 – 4×15 – 11.25× 10 - 5YB = 0  YB=10.5t 4) ∑Y = 0  30 – 4 – 11.25 – 10.5 – YA=0 YA=4.25t
= 0 = X d  × 8 – 8 × 2 X d  = 2 t   = 8  ×12 + 2.5 × 12 × 6 Xd -  2  × 8 - 10 ×Y d =0 Y d  =   26 t ∑ Y = 0 = Y a  + 26 – 2.5 × 12 – 8  Y a  = 30 + 8 – 26 = 12 t.  ∑ X = 0 = X a  – 0.5 × 8 – 2  Xa = 4 + 2 = 6 t. ←  Solution of Example 9
= 0 = Ma + 0.5 × 8 × 4 – 6 × 8  M a  = 48 – 16 = 32 m.t (anticlockwise) Check :  ∑Mc for part ac   Xa  Ya 32 + 0.5 × 8 × 4 + 2.5 × 12 × 4 –  6  × 8 –  12  × 10 = 32 + 16 + 120 – 48 – 120 = 0 Solution of Example 9 “Continued”
1) ∑MF(right) = 0   RC cosα × 4.5 – 4 × 4.5 × 2.25 – 10 × 10.5 = 0 RC = 40.4 t  2) ∑MA = 0 YB×9 + XB × 2 + RC cosα × 18 + RC sinα × 8 –10×24    - 20×4.5 – 5 × 5 – 4 × 9 × 13.5 + 5 × 2 = 0    4.5 YB = 27.57 – XB  (1) 3) ∑ME (right) = 0 4.5 YB - 6XB + RC cosα × 13.5 – 4 × 9 × 9 - 10 × 19.5 = 0   4.5 YB = 6XB + 82. 545  (2) Solution of Example 10
By solving equations (1) & (2) we get YB = 7.87 t. XB= - 7.85t 4) ∑Y  = 0  YA = 36 + 10 + 20 + 5 – 32.33 – 7.87 YA = 30.8 t. 5) ∑ME(left) = 0  4.5 YA – 8 XA – 5 × 3 – 5 × 6.5 = 0 XA = 11.4 t. Solution of Example 10 “Continued”
[object Object],[object Object],[object Object],A  Stable  Structure   is one that support : a system of loads.  These loads together with the support reactions have to be in  equilibrium and satisfy the three equilibrium  equations  in addition to  conditional equations (if any). Stability of Structures   Statically  Unstable  Structure is one in which: the number of the unknown  reactions is  less than  the  sum of the   available equilibrium and conditional equations (if any).
Externally Statically Unstable Structures Geometrical Unstable Structures
Statically  Determinate  Structure is one in which t he reactions can be determined by application of the equations of  equilibrium in addition to conditional equations(if any).   Determinancy of Structures   Statically  Indeterminate  Structure is one in which the number of  unknown reactions is  more than  the number  of available equations Stable-Once Statically Indeterminate Stable-Three Times Statically Indeterminate
Check the stability and determinacy for the following structures. Then, show how to modify it for stability  and determinancy  (a) (b) (c) (d) Solution of Example 11
Structure (a)   : Is unstable because there are only two  unknown reactions. The modification   :  Change either of the two roller supports to a hinge.
Structure (b)  :  Is unstable because the beam is rested on four link members connected at a point. The modification  :  Separate the link members   Modification for structure (b)
Structure (C)  :  Is stable and  three times statically indeterminate  because there are six  unknown support reactions. The modification  :  Add three intermediate hinges Modification for structure (C)
Structure (D)  :  Is stable and  five times statically  indeterminate  because there are  8 unknown support reactions  The modification :   One of fixed supports is changed to a roller  In addition to three  intermediate hinges  arranged as given in Struc. (c).

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Struc lec. no. 1

  • 1. Theory of Structures(1) Lecture No. 1
  • 2.
  • 3.
  • 4.
  • 5.
  • 6.
  • 7.
  • 9.
  • 10. Y B X A Y A Solution of Example 1 1- ∑ X = 0 XA – 5 = 0 XA = 5t 2- ∑MB = 0 YA × 6 – 2 × 6 × 3 + (4 × 3)/2 × 1 = 0 YA= 5t 3- ∑ Y = 0 YA + YB = 2 × 6+ (4 × 3)/2=18 YB = 13t
  • 11. Solution of Example 2 1-      ∑ X = 0 X A = 3t 2-      ∑ M B = 0 Y A × 4 + 8 + 4 × 1 – 3 × 1= 0 Y A = -2.25t ↑ Y A =2.25t ↓ 3- ∑ y = 0 Y A + 2× 2 = Y B 2.25+ 4 = Y B Y B = 6.25 t ↑ Y A X A Y B
  • 12. Solution of Example 3 1- ∑ X = 0 XB – 4 = 0 XB = 4t 2- ∑ MA = 0 10YB – 4 × 12 – 2 × 9 – 2 × 5× 2.5 – 4 × 3= 0 YB = 10.3 t 3- ∑ Y = 0 YA + YB = 4 + 2 + 10 = 16 YA = 5.7 t Y B Y A X B
  • 13. Solution of Example 4 1- ∑ X = 0 XA – 4 = 0 XA = 4t 2- ∑ Y = 0 YA – 1 × 6 – 5 – 5 – 2.5 = 0 YA = 18.5 t 3- ∑ M / A = 0 MA – 5 × 2 – 5 × 4 – 2.5 ×6 - 1×6×3 = 0 M A = 63 t.m
  • 14. Solution of Example 5 R 1 = 1/2 × 4 × 8 = 16 t R 2 = 0.5 × 4 = 2 t 1- ∑ X = 0 X A – R 2 = 0 X A = 2t 2- ∑ M A = 0 11 Y B + 2 × 13 – R 2 × 2 – 2 × 1 – R 1 × 7= 0 Y B = 8.36 t 3- ∑ Y = 0 Y A + Y B + 2 – 2 – 16 = 0 YA= 7.64t
  • 15. Solution of Example 6 1- ∑ X = 0 X B – 20 = 0 X B = 20t 2- ∑ M A = 0 6 Y B + 20 × 3 – 10 × 6 – 20 × 6 = 0  Y B = 20t 3- ∑Y = 0 Y A + Y B = 20 + 30 + 10 = 60  Y A = 40t
  • 16. Solution of Example 7 ∑ MO = 0 3 × 0 + 8 × 1 + 1 × 3 – Rd × 5 = 0 Rd = 2.2 t ↑ ∑ Mp = 0 1 × 2 + 8 × 4 + 3 × 5 – Rb × 5 = 0 Rb = 6.93t ∑ Mq = 0 1 × 2 + 8 × 4 + 3 × 5 – Rc × 5 = 0 Rc = 6.93t 8t
  • 17.
  • 18. Solution of Example 8 Method I 1- Part FD 1) ∑ MD = 0 8 × 2 = 4 YF YF = 4t 2) ∑Y = 0 YD = 8 – 4 YD = 4t 2- Part ECF 1) ∑ ME = 0 10×2.5+4×5= 4YC YC= 11.25t 2) ∑Y = 0 YE=10+4-11.25 YE=2.75t 3- Part ABE 1) ∑MA=0 12×3+2.75×6=5YB YB=10.5t 2) ∑Y = 0 YA= 2.75 + 12-10.5 YA= 4.25t
  • 19. Solution of Example 8 “ Continued ” Method II 1)∑MF(right)= 0 8 × 2 – 4 YD = 0 YD = 4t 2) ∑ME(right)= 0 18×4.5 – 4×9 – 4YC= 0 YC=11.25t 3) ∑MA = 0 30×7.5 – 4×15 – 11.25× 10 - 5YB = 0 YB=10.5t 4) ∑Y = 0 30 – 4 – 11.25 – 10.5 – YA=0 YA=4.25t
  • 20. = 0 = X d × 8 – 8 × 2 X d = 2 t  = 8 ×12 + 2.5 × 12 × 6 Xd - 2 × 8 - 10 ×Y d =0 Y d = 26 t ∑ Y = 0 = Y a + 26 – 2.5 × 12 – 8 Y a = 30 + 8 – 26 = 12 t. ∑ X = 0 = X a – 0.5 × 8 – 2 Xa = 4 + 2 = 6 t. ← Solution of Example 9
  • 21. = 0 = Ma + 0.5 × 8 × 4 – 6 × 8 M a = 48 – 16 = 32 m.t (anticlockwise) Check : ∑Mc for part ac Xa Ya 32 + 0.5 × 8 × 4 + 2.5 × 12 × 4 – 6 × 8 – 12 × 10 = 32 + 16 + 120 – 48 – 120 = 0 Solution of Example 9 “Continued”
  • 22. 1) ∑MF(right) = 0 RC cosα × 4.5 – 4 × 4.5 × 2.25 – 10 × 10.5 = 0 RC = 40.4 t 2) ∑MA = 0 YB×9 + XB × 2 + RC cosα × 18 + RC sinα × 8 –10×24 - 20×4.5 – 5 × 5 – 4 × 9 × 13.5 + 5 × 2 = 0 4.5 YB = 27.57 – XB (1) 3) ∑ME (right) = 0 4.5 YB - 6XB + RC cosα × 13.5 – 4 × 9 × 9 - 10 × 19.5 = 0 4.5 YB = 6XB + 82. 545 (2) Solution of Example 10
  • 23. By solving equations (1) & (2) we get YB = 7.87 t. XB= - 7.85t 4) ∑Y = 0 YA = 36 + 10 + 20 + 5 – 32.33 – 7.87 YA = 30.8 t. 5) ∑ME(left) = 0 4.5 YA – 8 XA – 5 × 3 – 5 × 6.5 = 0 XA = 11.4 t. Solution of Example 10 “Continued”
  • 24.
  • 25. Externally Statically Unstable Structures Geometrical Unstable Structures
  • 26. Statically Determinate Structure is one in which t he reactions can be determined by application of the equations of equilibrium in addition to conditional equations(if any). Determinancy of Structures Statically Indeterminate Structure is one in which the number of unknown reactions is more than the number of available equations Stable-Once Statically Indeterminate Stable-Three Times Statically Indeterminate
  • 27. Check the stability and determinacy for the following structures. Then, show how to modify it for stability and determinancy (a) (b) (c) (d) Solution of Example 11
  • 28. Structure (a) : Is unstable because there are only two unknown reactions. The modification : Change either of the two roller supports to a hinge.
  • 29. Structure (b) : Is unstable because the beam is rested on four link members connected at a point. The modification : Separate the link members Modification for structure (b)
  • 30. Structure (C) : Is stable and three times statically indeterminate because there are six unknown support reactions. The modification : Add three intermediate hinges Modification for structure (C)
  • 31. Structure (D) : Is stable and five times statically indeterminate because there are 8 unknown support reactions The modification : One of fixed supports is changed to a roller In addition to three intermediate hinges arranged as given in Struc. (c).