Engineering Formulas and Allowable Stresses for Structural Members, Exercises of Structural Design and Architecture

Various engineering formulas for calculating forces, moments, stresses, and deflections of structural members. It also includes allowable stresses for different materials and member types according to aisc-lrfd and wood design codes.

Typology: Exercises

2011/2012

Uploaded on 12/22/2012

bageshri
bageshri 🇮🇳

4.3

(24)

175 documents

1 / 8

Toggle sidebar

This page cannot be seen from the preview

Don't miss anything!

bg1
1
Reference Formulas
=0
x
F
γ
cos2ABBAC 222 += A
Ax
x
ˆ
Σ
Σ
=
=0
y
F
γβα
sin
C
sin
B
sin
A==
=
== n
i
iiy AxAxQ
1
=0M
a
acbb
2
4
x
2±
= A
Ay
y
ˆ
Σ
Σ
=
θ
cosFFx= drp
ππ
== 2
=
== n
i
iix AyAyQ
1
θ
sinFFy= dtlWA == 2
AdII +=
22
yx FFF += 4
2
2d
rA
π
π
==
x
y
F
F
=
θ
tan FdM = A
I
r=
2
s
m
9.81 g = mgF = c
I
S=
w
dx =
dV bmxy += 2
4
c
J
π
=
V
dx =
dM
12
12
xx
yy
m
=
( )
2
44
io cc
J
=
π
2
m
N
Pa = 2
s
mkg
N
= °= 180)radians(π
Pa,kPa 00011 = 2
in
lb
psi = 2
in
kip
ksi =
2
11 m
kN
kPa = lbkip 10001 = ftin 112 =
PaMPa 6
101 = PaGPa 9
101 = mmm 10001 =
A
P
fc= allowable
ultimate
SF =. L
δ
ε
=
A
P
ft= A
P
fv= A
P
fv2
=
A
P
fp= J
T
ρ
τ
= td
P
A
P
fp==
I
My
fy= Ib
VQ
favev =
ε
Ef =
S
M
I
Mc
fmaxb ==
A
V
fmaxv 2
3
=
for a rectangle AE
PL
=
δ
b
req F
M
S dt
V
A
V
f
wweb
v=
max
for an I beam
LT
T)(
Δαδ
=
x
I
QV
VT
allongitudin Δ= E
fx
zy
μ
εε
== )( T
T
Δαε
=
2
AdII c+=
docsity.com
pf3
pf4
pf5
pf8

Partial preview of the text

Download Engineering Formulas and Allowable Stresses for Structural Members and more Exercises Structural Design and Architecture in PDF only on Docsity!

1

Reference Formulas

∑ Fx=^0 C^ A B 2ABcos^ γ

2 2 2 = + − A

xA ˆx

∑ Fy=^0

α β sin γ

C

sin

B

sin

A = =

=

= =

n

i

Qy xA xiAi 1

∑ M^ =^0

a

b b ac

2

4 x

2 − ± − = A

yA yˆ

F x = Fcos θ p= 2 π r= πd ∑

=

= =

n

i

Q (^) x yA yiAi 1

F (^) y = Fsin θ A = W⋅l=t⋅d I =I+ Ad^2

2 2 F = Fx +F y 4

2 2 d A r

π =π =

x

y

F

F tan θ = M = Fd A

I r =

2 s

g = 9.81m F = mg c

I

S =

w dx

=−

dV y = mx+b 2

4 c J

V dx

=

dM

2 1

2 1

x x

y y m −

( )

4 4 co c i J

2 m

N Pa = (^2) s

kg m N

⋅ = π (radians)=^180 °

1 kPa = 1 , 000 Pa 2 in

psi = lb 2 in

kip ksi =

(^1 ) m

kN kPa = 1 kip = 1000 lb 12 in = 1 ft

MPa Pa

6 1 = 10 GPa Pa

9 1 = 10 1 m^ =^1000 mm

A

P f (^) c = allowable

ultimate F .S = L

δ ε =

A

P f (^) t = A

P f (^) v = A

P f (^) v 2

=

A

P f (^) p = J

T ρ τ = td

P

A

P f (^) p = =

I

My f (^) y = Ib

VQ f (^) v −ave= f^ =E^ ε

S

M

I

Mc f (^) b −max= = A

V

f (^) v max 2

− = for a rectangle^ AE

PL δ =

b

req F

M S ≥ t d

V

A

V

f

web w

v −max ≅ = for an^ I^ beam^ δ^ T =α(^ Δ T ) L

x I

V Q V

T longitudinal =^ Δ E

f (^) x y z

μ ε = ε =− ε T^ =α(^ Δ T )

2 I =∑Ic +∑ Ad

p I

VQ nF

connectedarea connector ≥^ ⋅ L

f (^) v G

ρφ = τ = ⋅ L

ρφ γ =

2 c 1 ab

T τ (^) max = c ab G

TL 3 2

φ = JG

TL φ =

2 3

(^1) ab

T τ (^) max = ab G

TL 3 3

1

φ = 3 3

1 ii

max max bt

Tt

τ =

t a

T max 2

= i (^) i

i

t

s

t

TL 2

4 a

φ 3 3

1 G bi ti

TL

φ =

EI R

M

ρ

Δ = dx EI

M ( x) 2 n= b+ 3

PU = PL γ L+PD γ D≤ φP n

AISC-LRFD:

PU : 1.4D

M (^) u ≤φbMn= 0. 9 FyZ

L Kl e = PU : 1.2D +1.6L+0.5(LrorSorR) M (^) ult =Mp=fyΣAiyi= fyZ

2

2

2

2

r

L

π EA

L

π EI P

e e

cr PU: 1.2D+ 1.6(LrorSorR)+

(0.5L or 0.8W) S

k = Z

y

p

f

M

Z =

PU: 1.2D+ 1.3W+0.5L +

0.5(Lr orSor R)

c c

P F A.

u cr g

2

2

r

L

E

f

e

cr

V ( 0. 6 F A ) 0. 9

u v yw w v

E

F

r

Kl (^) y c

Wood:

F =CD CMCF ×F tabulated

′ K λ^ c≤^1.^5

Fcr ( )F y

c

2

  1. 658

λ

c c p c D p

F ′ =F C = FC C

λc > 1. 5 y

c

cr

F F

2

λ

2

⎟ ⎠

d

l

K E

F

e

cE cE

K (^) cE = 0.3 sawn, 0.418 glulam

P

P

c n

u ≥ 02 φ

M

M

M

M

P

P

b ny

uy

b nx

ux

c n

u ≤ ⎟

φ φ φ

2

F

f F

f

F

f

cEx

c bx

bx

c

c

P

P

c n

u < 02

M

M

M

M

P

P

b ny

uy

b nx

ux

c n

u ≤ ⎟

φ φ φ

I

Mc

A

P

f (^) max = + Pu^ ≤^ φt^ FyAg^ φt =^0.^9 Pu ≤φtFuAe φt= 0. 75

  • ≤ 1. 0

b

b

a

a

F

f

F

f

I

M z

I

M y

A

P

f

1 2 max =^ + +^1.^0 F

f

F

f

F

f

by

by

bx

bx

a

a

BOLTS, THREADED PARTS AND RIVETS

Allowable Shear in kips

-^ 25%

75%

75%

BOLTS, AND THREADED PARTS

Allowable Bearing load in kips