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(1)

lecture

twenty

steel construction:

columns & tension members

Cor-Ten Steel Sculpture By Richard Serra Museum of Modern Art Fort Worth, TX (AISC - Steel Structures of the Everyday)

A

RCHITECTURAL

S

TRUCTURES

:

F

ORM,

B

EHAVIOR, AND

D

ESIGN

A

RCH 331

HÜDAVERDİ TOZAN

(2)

Structural Steel

• standard rolled shapes

(W, C, L, T)

• tubing

• pipe

(3)

Design Methods (revisited)

• know

– loads or lengths

• select

– section or load

– adequate for

strength and

no buckling

(4)

Allowable Stress Design (ASD)

• AICS 9

th

ed

• slenderness ratio

– for kl/r



C

c

= 126.1 with F

y

= 36 ksi

= 107.0 with F

y

= 50 ksi

 

2

2

23

12

.

.

r

K l

E

S

F

f

F

a

cr i t i ca l

r

Kl

(5)

C

c

and Euler’s Formula

• Kl/r < C

c

– short and stubby

– parabolic transition

• Kl/r > C

c

– Euler’s relationship

– < 200 preferred

E

C

2

2

(6)
(7)

Short / Intermediate

• L

e

/r < C

c

– where

 

.

.

2

1

2

2

S

F

F

C

r

K l

F

y

c

a

   

3

3

8

8

3

3

5

.

.

c

c

C

r

K l

C

r

K l

S

F

(8)

Unified Design

• limit states for failure

1. yielding

2. buckling

F

e

– elastic buckling stress (Euler)

g

c r

n

c

0

.

9 0

P

F

A

n

a

P

P

n

c

u

P

P

y

e

y

F

.

F

or

F

E

.

r

K L

44

0

71

4

y

e

y

F

.

F

or

F

E

.

r

K L

44

0

71

4

(9)

Unified Design

• P

n

= F

cr

A

g

– for

– for

– where

y

F

F

cr

y

F

.

F

F

E

.

r

KL

e

y

4

71

0

658

e

cr

y

F

.

F

F

E

.

r

K L

877

0

71

4

 

2

2

r

KL

E

F

e

(10)

Procedure for Analysis

1. calculate KL/r

biggest of KL/r with respect to x axes and y axis

2. find F

a

or F

cr

from appropriate equation

tables are available

3. compute P

allowable

= F

a

A or P

n

= F

cr

A

g

or find f

actual

= P/A

4. is P

P

allowable

(P

a

P

n

/

)? or is P

u

P

n

?

yes: ok

(11)

1. guess a size (pick a section)

2. calculate KL/r

biggest of KL/r with respect to x axes and y axis

3. find F

a

or F

cr

from appropriate equations

or find a chart

4. compute P

allowable

= F

a

A (P

n

/

= F

cr

A

g

)

or P

n

= F

cr

A

g

or find f

actual

= P/A

(12)

Procedure for Design (cont’d)

5. is P

P

allowable

(P

a

P

n

/

)? or is P

u

P

n

?

yes: ok

no: pick a bigger section and go back to step 2.

6. check design efficiency

percentage of stress =

if between 90-100%: good

if < 90%: pick a smaller section and

go back to step 2.

%

P

P

c

r

100

(13)
(14)
(15)
(16)

Beam-Column Design

• moment magnification (P-

)

C

m

– modification factor for end conditions

= 0.6 – 0.4(M

1

/M

2

) or

0.85 restrained, 1.00 unrestrained

P

e1

– Euler buckling strength

)

P

/

P

(

C

B

e

u

m

1

1

1

f a c t o r e d

m a x

u

B

M

M

1

 

2

2

1

r

Kl

EA

P

e

(17)

Beam-Column Design

• LRFD (Unified) Steel

– for

– for

P

r

is required, P

c

is capacity

c

- resistance factor for compression = 0.9

- resistance factor for bending = 0.9

0

1

9

8

2

0

.

M

M

M

M

P

P

:

.

P

P

n x

b

u x

n x

b

u x

n

c

u

c

r





0

1

2

2

0

.

M

M

M

M

P

P

:

.

P

P

n x

b

u x

n x

b

u x

n

c

u

c

r





(18)

Design Steps Knowing Loads

(revisited)

1. assume limiting stress

buckling, axial stress,

combined stress

2. solve for r, A or S

3. pick trial section

4. analyze stresses

5. section ok?

(19)

Rigid Frame Design

(revisited)

• columns in frames

– ends can be “flexible”

– stiffness affected by beams

and column = EI/L

– for the joint

• l

c

is the column length of each column

• l

b

is the beam length of each beam

b

c

l

EI

l

EI

G

(20)

Rigid Frame Design

(revisited)

• column effective length, k

A

(21)

• steel members can

have holes

• reduced area

• increased stress

Tension Members

(AISC - Steel Structures of the Everyday)

g

s

t

A

A

A

n

g

of

all

holes

4

2

(22)

Effective Net Area

• likely path to “rip” across

• bolts divide transferred force too

• shear lag

A

A

U

n

e

(23)

Tension Members

• limit states

for failure

1. yielding

2. rupture*

A

g

- gross area

A

e

- effective net area

(holes 1/8” + d)

F

u

= the tensile strength

n

a

P

P

P

u

t

P

n

g

y

n

t

0

.

9 0

P

F

A

e

u

n

t

0

.

7 5

P

F

A

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