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ME 101: Engineering Mechanics Rajib Kumar Bhattacharjya Department - - PowerPoint PPT Presentation

ME 101: Engineering Mechanics Rajib Kumar Bhattacharjya Department of Civil Engineering Indian Institute of Technology Guwahati M Block : Room No 005 : Tel: 2428 www.iitg.ernet.in/rkbc Equilibrium of rigid body Equations of equilibrium become


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SLIDE 1

ME 101: Engineering Mechanics

Rajib Kumar Bhattacharjya

Department of Civil Engineering Indian Institute of Technology Guwahati M Block : Room No 005 : Tel: 2428 www.iitg.ernet.in/rkbc

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SLIDE 2

Equilibrium of rigid body

  • =

= =

A y x

M F F Equations of equilibrium become There are three unknowns and number of equation is three. Therefore, the structure is statically determinate The rigid body is completely constrained

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SLIDE 3

Equilibrium of rigid body

More unknowns than equations Fewer unknowns than equations, partially constrained Equal number unknowns and equations but improperly constrained

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SLIDE 4

Example problem 1

A fixed crane has a mass of 1000 kg and is used to lift a 2400 kg crate. It is held in place by a pin at A and a rocker at B. The center of gravity of the crane is located at G. Determine the components of the reactions at A and B. SOLUTION:

  • Create a free-body diagram for the crane.
  • Determine B by solving the equation

for the sum of the moments of all forces about A. Note there will be no contribution from the unknown reactions at A.

  • Determine the reactions at A by

solving the equations for the sum of all horizontal force components and all vertical force components.

  • Check the values obtained for the

reactions by verifying that the sum of the moments about B of all forces is zero.

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SLIDE 5

Example problem 4

A sign of uniform density weighs 1200-N and is supported by a ball- and-socket joint at A and by two cables. Determine the tension in each cable and the reaction at A. SOLUTION:

  • Create a free-body diagram for the sign.
  • Apply the conditions for static

equilibrium to develop equations for the unknown reactions.

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SLIDE 6

Example problem 4

  • Create a free-body diagram for the

sign. Since there are only 5 unknowns, the sign is partially constrain. It is free to rotate about the x axis. It is, however, in equilibrium for the given loading.

( ) ( )

k j i T k j i T r r r r T T k j i T k j i T r r r r T T

EC EC E C E C EC EC BD BD B D B D BD BD

  • 285

. 428 . 85 . 1 . 2 6 . 9 . 8 . 1 6 . 3 4 . 2 2 . 1 4 . 2

3 2 3 1 3 2

+ + − = + + − = − − = − + − = − + − = − − =

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SLIDE 7

Example problem 4

  • Apply the conditions for

static equilibrium to develop equations for the unknown reactions.

( ) ( ) ( )

m . N 1440 771 . 8 . : 514 . 6 . 1 : N 1200 m 1.2 29 . 67 . : N 1200 43 . 33 . : 86 . 67 . : N 1200 = − + = − = − × + × + × = = + − = − + + = − − = − + + =

  • EC

BD EC BD EC E BD B A EC BD z EC BD y EC BD x EC BD

T T k T T j j i T r T r M T T A k T T A j T T A i j T T A F

  • (

) ( ) ( )k

j i A T T

EC BD

  • N

100.1 N 419 N 1502 N 1402 N 451 − + = = = Solve the 5 equations for the 5 unknowns,

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SLIDE 8

Structural Analysis

Engineering Structure

An engineering structure is any connected system of members built to support or transfer forces and to safely withstand the loads applied to it.

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SLIDE 9

Structural Analysis

Statically Determinate Structures

To determine the internal forces in the structure, dismember the structure and analyze separate free body diagrams of individual members or combination of members.

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SLIDE 10

Structural Analysis: Plane Truss

Truss: A framework composed of members joined at their ends to form a rigid structure Joints (Connections): Welded, Riveted, Bolted, Pinned

Plane Truss: Members lie in a single plane

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SLIDE 11

Structural Analysis: Plane Truss

Simple Trusses Basic Element of a Plane Truss is the Triangle

  • Three bars joined by pins at their ends Rigid Frame

– Non-collapsible and deformation of members due to induced internal strains is negligible

  • Four or more bars polygon Non-Rigid Frame

How to make it rigid or stable?

Structures built from basic triangles Simple Trusses

by forming more triangles!

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SLIDE 12

Structural Analysis: Plane Truss

Basic Assumptions in Truss Analysis All members are two-force members. Weight of the members is small compared with the force it supports (weight may be considered at joints) No effect of bending on members even if weight is considered

External forces are applied at the pin connections Welded or riveted connections Pin Joint if the member centerlines are concurrent at the joint

Common Practice in Large Trusses Roller/Rocker at one end. Why?

  • to accommodate deformations due to

temperature changes and applied loads.

  • therwise it will be a statically indeterminate

truss

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SLIDE 13

Structural Analysis: Plane Truss

Truss Analysis: Method of Joints

  • Finding forces in members

Method of Joints: Conditions of equilibrium are satisfied for the forces at each joint

– Equilibrium of concurrent forces at each joint – only two independent equilibrium equations are involved Steps of Analysis

1.Draw Free Body Diagram of Truss 2.Determine external reactions by applying equilibrium equations to the whole truss 3.Perform the force analysis of the remainder

  • f the truss by Method of Joints
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SLIDE 14

Structural Analysis: Plane Truss

Method of Joints

  • Start with any joint where at least one known load exists and where not

more than two unknown forces are present.

FBD of Joint A and members AB and AF: Magnitude of forces denoted as AB & AF

  • Tension indicated by an arrow away from the pin
  • Compression indicated by an arrow toward the pin

Magnitude of AF from Magnitude of AB from Analyze joints F, B, C, E, & D in that order to complete the analysis

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SLIDE 15

Structural Analysis: Plane Truss

Method of Joints

  • Negative force if assumed

sense is incorrect

Zero Force Member Check Equilibrium Show forces on members

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SLIDE 16

Method of Joints: Example

Determine the force in each member of the loaded truss by Method of Joints

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SLIDE 17

Method of Joints: Example

Solution

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SLIDE 18

Method of Joints: Example

Solution

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SLIDE 19

Structural Analysis: Plane Truss

When more number of members/supports are present than are needed to prevent collapse/stability Statically Indeterminate Truss

  • cannot be analyzed using equations of equilibrium alone!
  • additional members or supports which are not necessary for

maintaining the equilibrium configuration Redundant

Internal and External Redundancy

Extra Supports than required External Redundancy

– Degree of indeterminacy from available equilibrium equations

Extra Members than required Internal Redundancy

(truss must be removed from the supports to calculate internal redundancy) – Is this truss statically determinate internally?

Truss is statically determinate internally if m + 3 = 2j m = 2j – 3 m is number of members, and j is number of joints in truss L06

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SLIDE 20

Structural Analysis: Plane Truss

Internal Redundancy or Degree of Internal Static Indeterminacy

Extra Members than required Internal Redundancy

Equilibrium of each joint can be specified by two scalar force equations 2j equations for a truss with “j” number of joints Known Quantities For a truss with “m” number of two force members, and maximum 3 unknown support reactions Total Unknowns = m + 3 (“m” member forces and 3 reactions for externally determinate truss) Therefore: m + 3 = 2jStatically Determinate Internally m + 3 > 2jStatically Indeterminate Internally m + 3 < 2jUnstable Truss

A necessary condition for Stability but not a sufficient condition since

  • ne or more members can be

arranged in such a way as not to contribute to stable configuration of the entire truss

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SLIDE 21

Structural Analysis: Plane Truss

To maintain alignment of two members during construction To increase stability during construction To maintain stability during loading (Ex: to prevent buckling

  • f compression members)

To provide support if the applied loading is changed To act as backup members in case some members fail or require strengthening Analysis is difficult but possible

Why to Provide Redundant Members?

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SLIDE 22

Structural Analysis: Plane Truss

Zero Force Members

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SLIDE 23

Structural Analysis: Plane Truss

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SLIDE 24

Structural Analysis: Plane Truss

Zero Force Members: Conditions

If only two non-collinear members form a truss joint and no external load or support reaction is applied to the joint, the two members must be zero force members If three members form a truss joint for which two of the members are collinear, the third member is a zero-force member provided no external force or support reaction is applied to the joint

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SLIDE 25

Structural Analysis: Plane Truss

Special Condition

When two pairs of collinear members are joined as shown in figure, the forces in each pair must be equal and opposite.

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SLIDE 26

Method of Joints: Example

Determine the force in each member of the loaded truss by Method of Joints. Is the truss statically determinant externally? Is the truss statically determinant internally? Are there any Zero Force Members in the truss? Yes Yes No

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SLIDE 27

Method of Joints: Example

Solution

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SLIDE 28

Method of Joints: Example

Solution

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SLIDE 29
  • DETERMINATE

INDETERMINATE INDETERMINATE DETERMINATE INDETERMINATE DETERMINATE

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SLIDE 30

Example problem 1

  • Create the free-body diagram.

Determine B by solving the equation for the sum of the moments of all forces about A.

( ) ( ) ( )

m 6 kN 5 . 23 m 2 kN 81 . 9 m 5 . 1 : = − −

  • +

= B M A kN 1 . 107 + = B Determine the reactions at A by solving the equations for the sum of all horizontal forces and all vertical forces. : = + =

  • B

A F

x x

kN 1 . 107 − =

x

A kN 5 . 23 kN 81 . 9 : = − − =

  • y

y

A F kN 3 . 33 + =

y

A

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SLIDE 31

Example problem 2

A loading car is at rest on an inclined

  • track. The gross weight of the car and

its load is 25 kN, and it is applied at

  • G. The cart is held in position by the

cable. Determine the tension in the cable and the reaction at each pair of wheels. SOLUTION:

  • Create a free-body diagram for the car

with the coordinate system aligned with the track.

  • Determine the reactions at the wheels

by solving equations for the sum of moments about points above each axle.

  • Determine the cable tension by

solving the equation for the sum of force components parallel to the track.

  • Check the values obtained by verifying

that the sum of force components perpendicular to the track are zero.

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SLIDE 32

Example problem 2

Create a free-body diagram

( ) ( )

kN 10.5 25 sin kN 25 kN 22.65 25 cos kN 25 − = − = + = + =

  • y

x

W W

Determine the reactions at the wheels.

( ) ( ) ( )

mm 1250 mm 150 kN 22.65 mm 625 kN 10.5 :

2

= + − − =

  • R

M A

kN 8

2

+ = R

( ) ( ) ( )

mm 1250 mm 150 kN 22.65 mm 625 kN 10.5 :

1

= − − + =

  • R

M B

kN 2.5

1 =

R

Determine the cable tension.

T kN 22.65 : = − + =

  • x

F

kN 22.7 + = T

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SLIDE 33

Example problem 3

A 6-m telephone pole of 1600-N used to support the wires. Wires T1 = 600 N and T2 = 375 N. Determine the reaction at the fixed end A. SOLUTION:

  • Create a free-body diagram for the

telephone cable.

  • Solve 3 equilibrium equations for the

reaction force components and couple at A.

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SLIDE 34

Example problem 3

  • Create a free-body diagram for

the frame and cable.

  • Solve 3 equilibrium equations for the

reaction force components and couple.

10 cos ) N 600 ( 20 cos ) N 375 ( : = ° − ° + =

  • x

x

A F

N 238.50 + =

x

A

( ) ( )

20 sin N 375 10 sin 600N N 1600 : = ° − ° − − =

  • y

y

A F

N 1832.45 + =

y

A

  • =

:

A

M

( ) ( )

(6m) 20 cos 375N ) 6 ( 10 cos 600N = ° − ° + m M A

N.m 00 . 1431 + =

A

M

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SLIDE 35

Example

Using the method of joints, determine the force in each member of the truss. SOLUTION:

  • Based on a free-body diagram of the

entire truss, solve the 3 equilibrium equations for the reactions at E and C.

  • Joint A is subjected to only two unknown

member forces. Determine these from the joint equilibrium requirements.

  • In succession, determine unknown

member forces at joints D, B, and E from joint equilibrium requirements.

  • All member forces and support reactions

are known at joint C. However, the joint equilibrium requirements may be applied to check the results.

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SLIDE 36

Example

SOLUTION:

  • Based on a free-body diagram of the entire truss,

solve the 3 equilibrium equations for the reactions at E and C.

( )( ) ( )( ) ( )

m 3 m 6 kN 5 m 12 kN 10 E M C − + = =

= kN 50 E

  • =

=

x x

C F =

x

C

  • +

+ − = =

y y

C F kN 50 kN 5

  • kN

10

↓ = kN 35

y

C

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SLIDE 37

Example

  • Joint A is subjected to only two unknown

member forces. Determine these from the joint equilibrium requirements.

5 3 4 kN 10

AD AB

F F = =

C F T F

AD AB

kN 5 . 12 kN 5 . 7 = =

  • There are now only two unknown member

forces at joint D.

( ) DA

DE DA DB

F F F F

5 3

2 = = C F T F

DE DB

kN 15 kN 5 . 12 = =

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SLIDE 38

Example

  • There are now only two unknown member

forces at joint B. Assume both are in tension.

( )

kN 75 . 18 kN 12 kN 5

5 4 5 4

− = − − − = =

  • BE

BE y

F F F

C FBE kN 75 . 18 = ( ) ( )

kN 25 . 26 75 . 18 kN 5 . 12 kN 5 . 7

5 3 5 3

+ = − − − = =

  • BC

BC x

F F F

T FBC kN 25 . 26 =

  • There is one unknown member force at joint
  • E. Assume the member is in tension.

( )

kN 75 . 43 kN 75 . 18 kN 15

5 3 5 3

− = + + = =

  • EC

EC x

F F F C FEC kN 75 . 43 =

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SLIDE 39

Example

  • All member forces and support reactions are

known at joint C. However, the joint equilibrium requirements may be applied to check the results.

( ) ( ) ( ) ( )

checks 75 . 43 35 checks 75 . 43 25 . 26

5 4 5 3

= + − = = + − =

  • y

x

F F

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SLIDE 40

L 5

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SLIDE 41

Structural Analysis: Plane Truss

Method of Joints: only two of three equilibrium

equations were applied at each joint because the procedures involve concurrent forces at each joint Calculations from joint to joint More time and effort required

Method of Sections

Take advantage of the 3rd or moment equation of equilibrium by selecting an entire section of truss Equilibrium under non-concurrent force system Not more than 3 members whose forces are unknown should be cut in a single section since we have only 3 independent equilibrium equations

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SLIDE 42

Structural Analysis: Plane Truss

Method of Sections

Find out the reactions from equilibrium of whole truss To find force in member BE Cut an imaginary section (dotted line) Each side of the truss section should remain in equilibrium For calculating force on member EF, take moment about B Now apply

= 0 to obtain forces on the members BE

Take moment about E, for calculating force BC

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SLIDE 43

Structural Analysis: Plane Truss

Method of Sections

  • Principle: If a body is in equilibrium, then any part of the body is also in

equilibrium.

  • Forces in few particular member can be directly found out quickly without solving

each joint of the truss sequentially

  • Method of Sections and Method of Joints can be conveniently combined
  • A section need not be straight.
  • More than one section can be used to solve a given problem
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SLIDE 44

( )( ) ( )( ) ( )( ) ( )( ) ( )( ) ( )

↑ = + + − = = ↑ = + − − − − − = =

  • kN

5 . 12 kN 20 kN 5 . 7 m 30 kN 1 m 25 kN 1 m 20 kN 6 m 15 kN 6 m 10 kN 6 m 5 A A L F L L M

y A

Find out the internal forces in members FH, GH, and GI Find out the reactions

Structural Analysis: Plane Truss

Method of Sections: Example

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SLIDE 45
  • Pass a section through members FH, GH, and

GI and take the right-hand section as a free body.

( )( ) ( )( ) ( )

kN 13 . 13 m 33 . 5 m 5 kN 1 m 10 kN 7.50 + = = − − =

  • GI

GI H

F F M

  • Apply the conditions for static equilibrium to determine the

desired member forces.

T FGI kN 13 . 13 =

Method of Sections: Example Solution

° = = = = 07 . 28 5333 . m 15 m 8 tan α α GL FG

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SLIDE 46

( )( ) ( )( ) ( )( ) ( )( )

kN 82 . 13 m 8 cos m 5 kN 1 m 10 kN 1 m 15 kN 7.5 − = = + − − =

  • FH

FH G

F F M α

C FFH kN 82 . 13 =

( ) ( )( ) ( )( ) ( )( )

kN 371 . 1 m 15 cos m 5 kN 1 m 10 kN 1 15 . 43 9375 . m 8 m 5 tan

3 2

− = = + + = ° = = = =

  • GH

GH L

F F M HI GI β β β

C FGH kN 371 . 1 =

Method of Sections: Example Solution

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SLIDE 47

Structural Analysis: Space Truss

Space Truss

L07

3-D counterpart of the Plane Truss Idealized Space Truss Rigid links connected at their ends by ball and socket joints

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SLIDE 48

Structural Analysis: Space Truss

Space Truss

6 bars joined at their ends to form the edges of a tetrahedron as the basic non-collapsible unit. 3 additional concurrent bars whose ends are attached to three joints on the existing structure are required to add a new rigid unit to extend the structure. If center lines of joined members intersect at a point Two force members assumption is justified Each member under Compression or Tension A space truss formed in this way is called a Simple Space Truss

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SLIDE 49

A necessary condition for Stability but not a sufficient condition since one or more members can be arranged in such a way as not to contribute to stable configuration of the entire truss

Structural Analysis: Space Truss

Static Determinacy of Space Truss

Six equilibrium equations available to find out support reactions If these are sufficient to determine all support reactions The space truss is Statically Determinate Externally Equilibrium of each joint can be specified by three scalar force equations 3j equations for a truss with “j” number of joints Known Quantities For a truss with “m” number of two force members, and maximum 6 unknown support reactions Total Unknowns = m + 6 (“m” member forces and 6 reactions for externally determinate truss) Therefore: m + 6 = 3jStatically Determinate Internally m + 6 > 3jStatically Indeterminate Internally m + 6 < 3jUnstable Truss

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SLIDE 50

Structural Analysis: Space Truss

Method of Joints

  • If forces in all members are required
  • Solve the 3 scalar equilibrium equations at each joint
  • Solution of simultaneous equations may be avoided if a joint having at least one known force &

at most three unknown forces is analysed first

  • Use Cartesian vector analysis if the 3-D geometry is complex (F=0)

Method of Sections

  • If forces in only few members are required
  • Solve the 6 scalar equilibrium equations in each cut part of truss
  • Section should not pass through more than 6 members whose forces are unknown
  • Cartesian vector analysis (F=0, M=0)
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SLIDE 51

Space Truss: Example

Determine the forces acting in members

  • f the space truss.

Solution: Start at joint A: Draw free body diagram Express each force in vector notation

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SLIDE 52

Space Truss: Example

Rearranging the terms and equating the coefficients of i, j, and k unit vector to zero will give: Next Joint B may be analysed.

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SLIDE 53

Space Truss: Example

Using Scalar equations of equilibrium at joints D and C will give: Joint B: Draw the Free Body Diagram Scalar equations of equilibrium may be used at joint B

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SLIDE 54

Example problem

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SLIDE 55

Example problem

  • =
  • =

From similar triangle OFD and OGC, We have