roof truss problem

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Problem 6.37 The truss supports loads at A and H. Use the method of sections to determine the axial forces in members CE, BE, and BD. A B C D E F G H 300 mm 400 mm 18 kN 24 kN 400 mm 400 mm 400 mm Solution: First find the external support loads on the truss 18 kN 24 kN C D E G B X B Y F Y H 0.8 m 1.2 m 0.4 m F x : B x D 0 F y : B y C F y 18 24 D 0 (kN) M B : 0.8F y 1.224 C 0.418 D 0 Solving: B x D 0 B y D 15 kN F y D 27 kN Method of sections: 18 kN C CE E BD B Y 0.4 m 0.3 m BE θ θ tan D 3 4 D 36.87 ° B y D 15 kN F x : CE C BE cos C BD D 0 F y : B y 18 C BE sin D 0 C M B : C 0.418 0.3CE D 0 Solving, CE D 24 kN T BE D 5 kN T BD D28 kN C c 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as they currently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher. 1

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roof truss problem

Transcript of roof truss problem

Page 1: roof truss problem

Problem 6.37 The truss supports loads at A and H.Use the method of sections to determine the axial forcesin members CE, BE, and BD.

A

B

C

D

E

F

G H

300 mm

400 mm

18 kN 24 kN

400 mm 400 mm 400 mm

Solution: First find the external support loads on the truss

18 kN24 kN

C

D

E G

BX

BYFY

H

0.8 m

1.2 m

0.4 m

∑Fx : Bx D 0

∑Fy : By C Fy % 18 % 24 D 0 (kN)

∑MB: 0.8Fy % .1.2-.24- C .0.4-18 D 0

Solving: Bx D 0

By D 15 kN

Fy D 27 kN

Method of sections:

18 kN

C CE E

BD

BY

0.4 m

0.3 mBE

θ θ

tan & D 3

4

& D 36.87°

By D 15 kN∑Fx : CE C BE cos & C BD D 0

∑Fy : By % 18 C BE sin & D 0

C∑

MB: C .0.4-.18- % .0.3-.CE- D 0

Solving,CE D 24 kN .T-BE D 5 kN .T-BD D %28 kN .C-

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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Page 2: roof truss problem

Problem 6.49 Use the method of sections to determinethe axial force in member EF.

4 ft

4 ft

4 ft

4 ft

A

C

E

G

I

12 ft

D

B

F

H

10 kip

10 kip

Solution: The included angle at the apex BAC is

˛ D tan%1

(12

16

)D 36.87°.

The interior angles BCA, DEC, FGE, HIG are % D 90° % ˛ D 53.13°.The length of the member ED is LED D 8 tan ˛ D 6 ft. The interiorangle DEF is

ˇ D tan%1

(4

LED

)D 33.69°.

The complete structure as a free body: The moment about H is MH D%105124 % 105164 C I5124 D 0, from which I D 280

12D 23.33 kip.

The sum of forces:∑Fy D Hy C I D 0,

from which Hy D %I D %23.33 kip.

∑Fx D Hx C 20 D 0,

from which Hx D %20 kip. Make the cut through EG, EF, and DE.Consider the upper section only. Denote the axial force in a memberjoining I, K by IK. The section as a free body: The sum of the momentsabout E is ME D %10544 % 10584 C DF5LED4 D 0, from which DF D120

6D 20 kip.

The sum of forces:∑Fy D %EF sin ˇ % EG sin % % DF D 0,

∑Fx D %EF cos ˇ C EG cos % C 20 D 0,

from which the two simultaneous equations: 0.5547EF C 0.8EG D%20, and 0.8320EF % 0.6EG D 20. Solve: EF D 4.0 kip (T)

F = 10 kip

F = 10 kip

DF EF EG

Eβ γ

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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Page 3: roof truss problem

Problem 6.79 The frame supports a 6-kN load at C.Determine the reactions on the frame at A and D.

0.4 m0.8 m

A B

D EF

C

0.5 m

0.4 m 1.0 m6 kN

Solution: Note that members BE and CF are two force members.Consider the 6 kN load as being applied to member ABC.

Ax

Ay

FCFFBE

B C

0.4 m

1.0 m6 kN

θ φ

tan & D 0.5

0.4& D 51.34°

tan * D 0.5

0.2* D 68.20°

Member DEF

Dx

Dy

FCFFBE

FE

0.8 m 0.4 m

θφ

Equations of equilibrium:

Member ABC:∑Fx : Ax C FBE cos & % FCF cos * D 0

∑Fy : Ay % FBE sin & % FCF sin * % 6 D 0

C∑

MA: % /0.4.FBE sin & % /1.4.FCF sin * % 1.4/6. D 0

Member DEF:∑Fx : Dx % FBE cos & C FCF cos * D 0

∑Fy : Dy C FBE sin & C FCF sin * D 0

C∑

MD: /0.8./FBE sin &. C 1.2FCF sin * D 0

Unknowns Ax, Ay, Dx, Dy, FBE, FCF we have 6 eqns in 6unknowns.

Solving, we get

Ax D %16.8 kNAy D 11.25 kNDx D 16.3 kNDy D %5.25 kN

Also, FBE D 20.2 kN /T.

FCF D %11.3 kN /C.

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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Page 4: roof truss problem

Problem 6.85 Determine the forces on member ABC.

1 m

D C

E

A B

1 m

2 m 2 m 1 m

6 kN

Solution: The frame as a whole: The equations of equilibrium are

∑FX D AX C EX D 0,

∑FY D AY C EY % 6000 N D 0,

and, with moments about E,∑ME D 2AX % .5-6000 D 0.

Solving for the support reactions, we get AX D 15,000 N and EX D%15,000 N. We cannot yet solve for the forces in the y direction at Aand E.

Member ABC: The equations of equilibrium are

∑FX D AX % BX D 0,

∑FY D AY % BY % CY D 0,

and summing moments about A,

∑MA D %2BY % 4CY D 0.

Member BDE: The equations of equilibrium are

∑FX D EX C DX C BX D 0,

∑FY D EY C DY C BY D 0,

and, summing moments about E,

∑ME D .1-DY C .1-DX C .2-BY C .2-BX D 0.

Member CD: The equations of equilibrium are

∑FX D %DX D 0,

∑FY D %DY C CY % 6000 D 0,

and summing moments about D,

∑MD D %.4-6000 C 3CY D 0.

Solving these equations simultaneously gives values for all of theforces in the frame. The values are AX D 15,000 N, AY D %8,000 N,BX D 15,000 N, BY D %16,000 N, CY D 8,000 N, DX D 0, andDY D 2,000 N.

EYEX E DY

DX

DX D

BXBY

DY

BX

AXAY BY

CY

CY

D

B

BA

C

C

6 kN

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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Page 5: roof truss problem

Problem 6.95 Determine the forces on member AD.

400 N

200 N

C

D

130 mm

400 mm

400 mm 400 mm

BA

Solution: Denote the reactions of the support by Rx and Ry . Thecomplete structure as a free body:

∑Fx D Rx % 400 D 0,

from which Rx D 400 N. The sum of moments:∑MA D 800C % 400+930* C 400+530* % 400+200* D 0,

from which C D 300 N.∑Fy D C C Ry % 400 % 200 D 0,

from which Ry D 300 N. Element ABC : The sum of the moments:

∑MA D %4By C 8C D 0,

from which By D 600 N. Element BD : The sum of the forces:

∑Fy D By % Dy % 400 D 0,

from which Dy D 200 N.

Element AD: The sum of the forces:∑Fy D Ay C Dy % 200 D 0,

from which Ay D 0: Element AD: The sum of the forces:

∑Fx D Ax C Dx D 0

and∑

MA D %400+200* C 800Dy % 400Dx D 0

Ax D %200 N, and Dx D 200 N.

Element BD: The sum of forces:∑Fx D Bx % Dx % 400 D 0

from which Bx D 600 N. This completes the solution of the nineequations in nine unknowns, of which Ax , Ay , Dx , and Dy are thevalues required by the Problem.

200 N

400 N

400 N

Dy

Dy

Bx

BxRx

Ax

AxAy

Ay

Ry By

By

Dx

Dx

C

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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Page 6: roof truss problem

Problem 6.106 The woman exerts 20-N forces on thehandles of the shears. Determine the magnitude of theforces exerted on the branch at A.

BAC

D

E

25 mm25 mm36 mm

65 mm 20 N

20 N

Solution: Assume that the shears are symmetrical.

Consider the 2 pieces CD and CE∑Fx D 0 ) Dx D Ex

∑Fy D 0 ) Dy D Ey

∑MC D 0 ) Dx D Ex D 0

20 N

20 NEy

Ex

C

Dx

Dy

Now examine CD by itself∑MC D %*20 N)*90 mm) C Dy*25 mm) D 0 ) Dy D 72 N

20 N

Cy

Cx

Dx = 0

Dy

Finally examine DBA∑MB : A*36 mm) % Dy*50 mm) D 0

Bx

Dx = 0By

Dy

A

Solving we find A D 100 N

c# 2005 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as theycurrently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

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