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Page 1: Frames, Statics

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PLANE STRUCTURES FRAMES – is a rigid structure which is made up of members at least one of which is not a two-force member.

q  To simply put it, in order to solve for the unknown forces in the frame, you need to draw the FBD of the frame and individual members in the right sequence.

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The compound beam shown below is pinned connected at B. Determine the reactions at its supports. Neglect its weight and thickness.

EXAMPLE 6-15

2 m 2 m 2 m

10 kN 4 kN/m

Dismember the beam into 2 segments

A B

C 3

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Entire Beam Bar AB

Bar BC

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i. Dismember the beam into 2 segments: (For Bar AB)

10 kN

3 4

Ax

Ay MA Bx

By 2 m

4 m

For bar BC

Entire Beam

Back given problem 4

Bx

By

8 kN

1 m

2 m

i. Dismember the beam into 2 segments: (For Bar BC)

Cy

For bar AB

Entire Beam (Summary)

Back given problem

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10 kN

3 4

Ax

Ay MA Bx

By 2 m

4 m

Bx

By

8 kN

1 m

2 m

Cy

For bar BC For bar AB

i. Dismember the beam into 2 segments:

Compute for the reactions

Segment BC Segment AB

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10 kN

3 4

Ax

Ay MA Bx

By 2 m

4 m

0)53)(10( =+− xx BkNA

;0=↑+ ∑ yF

→ ;0=∑+xF

0)54)(10( =−− yy BkNA

0)4()2)(54)(10( =−− mBkNM yA

;0=∑ AM

ii. Equations of Equilibrium (For segment AB)

Segment BC Back

Page 2: Frames, Statics

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Bx

By

8 kN

1 m

2 m

Cy

0=xB

;0=↑+ ∑ yF

→ ;0=∑+xF

08 =+− yy CkNB

0)2()1(8 =+− mCmkN y

;0=∑ BM

ii. Equations of Equilibrium (For segment BC)

Final Answer Back

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iii. Solving these equations, we obtain:

0)53)(10( =+− xx BkNA

0)54)(10( =−− yy BkNA

0)4()2)(54)(10( =−− mBkNM yA

0=xB

08 =+− yy CkNB

0)2()1(8 =+− mCmkN y

kNAx 6=

0=xB

kNCy 4=

kNAy 6=

kNBy 4=

kNmMA 32=

Review Problem Back

Next Problem

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EXAMPLE 6-16

Determine the horizontal and vertical components of force which the pin at C on member ABCD of the frame.

0.8 m 100 kg

1.6 m

0.4 m

1.6 m 0.4 m

F E C

B

A

D Draw the FBD of the frame

See the FBD

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i. FBD of the frame ABCD:

2 m

2.8 m

Dx

Ax

Ay

A

D

Dismember the beam into 3 segments Bar CF

Bar AD

Bar BE

Equation of Equilibrium for Entire Frame

F=981 N

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07.700 =− NAx

;0=↑+ ∑ yF

→ ;0=∑+xF

0)8.2()2(981 =+− mDmN x

;0=∑ AM

ii. Equations of Equilibrium (Entire Frame)

0981 =− NAy

2 m

2.8 m

Dx

Ax

Ay

A

D

Dismember the beam into 3 segments

Bar CF Bar AD Bar BE

F=981 N

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F

981 N

ii. Equations of Equilibrium (For Bar CEF)

0)45cos2.1734( =°−−− NCx

;0=↑+ ∑ yF

→ ;0=∑+xF

0)6.1)(45sin()2(981 =°−− mFmN B

;0=+ ∑ CMccw

0)45sin2.1734( =°−− NCy

C Cx

Cy

E

FB

45º

1.6 m 0.4 m

Bar ACD

Bar BE

Entire Frame

NCy 245−=

NCx 1230=

Page 3: Frames, Statics

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Dx

Ax

Ay

A

D

FB

Cx

Cy

0.8 m

1.6 m

0.4 m

FBD of bar ACD

Back Bar BE Entire Frame

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FBD of bar BE

45º

FB

FB

Bar ACD

Entire Frame

Bar CEF

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Dx

Ax

Ay

A

D

C Cx

Cy

E F

981 N FB

45º

45º

FB

FB

FB Cx

Cy

0.8 m

1.6 m

0.4 m

1.6 m 0.4 m

Review

Final Answer

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NCy 245−=

ii. Final Answers for Problem 6-16

NCx 1230=

Review Next Problem

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EXAMPLE 6-17

The smooth disk shown below is pinned connected at D and has a weight of 20 lbs. Neglect the weights of the other members, determine the horizontal and vertical components of reaction at pins B and D.

3.5 ft

3 ft

C D r=0.5 ft

A B

Member AB FBD of Entire Frame

Disk 18

3 ft

Cx

A

Dx

Dy

Bx

By

Dx

Dy

20 lb

ND

Bx

By 3 ft

ND

ii. Free Body Diagram (Entire Frame)

Member AB EQ of Equilibrium

Disk

Page 4: Frames, Statics

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3.5 ft

3 ft

C D

A

B

ii. Equations of Equilibrium (Entire Frame)

01.17 =− lbAx;0=↑+ ∑ yF

→ ;0=∑+xF

0)5.3()3(20 =+− ftCftlb x

;0=+ ∑ AMCCW

020 =− lbAy

lbCx 1.17=

lbAx 1.17=

lbAy 20=

Member AB Disk

Back

20 lb

Cx

Ax

Ay

20

ii. Equations of Equilibrium (Member AB)

3 ft

A Bx

By 3 ft

ND 01.17 =− xBlb

;0=↑+ ∑ yF

→ ;0=∑+xF

0)3()6(20 =+− ftNftlb D

;0=+ ∑ BMCCW

04020 =+− yBlblb

lbBx 1.17=

lbND 40=

lbBy 20=

Disk Back

Ax

Ay

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Dx

Dy

20 lb

ND

ii. Equations of Equilibrium (Disk)

0=xD

;0=↑+ ∑ yF

→ ;0=∑+xF

02040 =−− yDlblb

0=xD

lbDy 20=

Summary of Answers Review

Back

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ii. Final Answers for Problem 6-17

lbCx 1.17=

Review

lbAx 1.17=

lbAy 20=

lbBx 1.17=

lbND 40=

lbBy 20=

0=xD

lbDy 20=

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Solution:

Page 5: Frames, Statics

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Solution:

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Solution:

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Solution:

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Solution:

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