steel design Flashcards

1
Q

shape factors of sections

A

hollow circle - 1.27
circular plate - 1.7
diamond section- 2
triangular section- 2.34

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2
Q

Center of gravity of semi circles

A

semi circular line = 2R /pi
semi circular plate =4R/3pi
hemisphere = 3R/8

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3
Q

ultimate plastic load for propped cantiliver

A

11.656 Mp / L^2

hinge at x= 0.414 L

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4
Q

maximum permissible deflection in SSB

A

table 6 is 800:2007
elements succeptible to cracking = L/300
not succeptible to cracking = L /240
for cantiliver = L/150 and L/120

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5
Q

limiting grip length in lap joint

A

Lg < 5d
effect of bending stress can be ignored in above condition
8d >Lg > 5d , reduction factor required
Lg > 8d , redesign required

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6
Q

minimum pitch, guage , end distance

A

pitch/guage = 2.5 bolt
end = 1.5 hole
= 1.7 hole (for hand cut element)

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7
Q

maximum edge , pitch distance in welds and bolts

A

end distance = 12 t.e , e = sqrt(250/fy)
comp pitch distance = 12t or 200 mm
tension pitch distance = 16t or 200 mm
in case of staggered = 1.5* distances

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8
Q

maximum pitch of tack bolt

A

for plates, flats = 32 t or 300 mm
if exposed to weather 16t or 200 mm
for compression = 600mm or λ1 <40 , 0.6λ
for tension member = 1000 mm

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9
Q

bolt and bolt hole

A
dia = 6.06 sqrt(t)      Unwins formula
nominal dia : hole clearence
12 ~ 14 mm : 1mm
16 ~ 24 mm : 2mm 
 > 24 mm   : 3mm
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10
Q

slot welding size limitation

A

width of slot > 25mm or 3.t

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11
Q

long joints, weld and bolt unbuttening effects

A

L > 150 throat

L > 15 bolt

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12
Q

slenderness ratio limits of steel members

A

λ < 180 , compression member
λ < 180 , tension member, but stress reverse due to
live load
λ < 250 , for wind earthquake loads
λ < 350 Tension member but reversal of stress due to wind load
λ < 400 , for tension members

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13
Q

net tearing area of staggered bolting

A

[ B -n.D +(S^2) /4g ] * t

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14
Q

lug angle design

A
minimum bolts at lug > 2 bolt
number of bolts at locations 
n1 = Fconnect /Rv
n2= 1.4* Fout /Rv
n3= 1.2* Fout /Rv
n2 interconnecting bolt must start in advance
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15
Q

design of bolted connection

A
  1. find dia of bolt = 6.04 *sqrt(t)
  2. find rivit value
  3. find no of bolts required
  4. arrangement of bolts
  5. width and thickness of plates
  6. efficiency of joint (if asked)
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16
Q

design of lacing

A
1. spacing of lacing
 C /r.min  <50 or 0.7*λ
2. dimension of lacing
 t > L1 /40, or L1 /60 
 λl = K.L1 /r < 145 (K=0.7 for double lacing or welded )
3. Forces in Lacing
 V= 2.5% of Pu
 F = V/ N*sin()
4. Forces < strength compressive and tensile
 T= 0.9fu Anet /1.25
 T= Ag * fy /1.2
 C= fcd* Ag (fcd depends on λl)
5. tie plate or batten plate 
 Dend > 2.B
           > centroidal distance between main members
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17
Q

width of lacing bars

A
bolt dia mm - width of lacing bar
16 - 50
18  - 55
20- 60
22- 65
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18
Q

to prevent web crippling

A

A = a +2.5*h2

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19
Q

to prevent web buckling

A

find K.l /r =2.45d / tw
fcd *Ag > R
A= a + d (1:1 dispersion)

20
Q

condition of plastic , compact and semi compact rolled I-section

A

b/tf < 9.4 e
d /tw < 84e

compact
b/tf < 10.5 e
d /tw < 105e

semi compact
b/tf < 15.7 e
d /tw < 126e

21
Q

bolt grade 4.6

A

400 mpa strength

22
Q

Kb in bearing of bolt

A

Kb =min [e/3d , p/3d -0.25, fub/fu, 1]

23
Q

rivit hole size

A
d' = d+ 1.5     for d<25
d' = d + 2      for d>25
24
Q

carbon content in mild steel

25
characterstics of steel used as plasstic steel
fy < 450 Mpa fu/fy > 1.2 εplastic > 1.15*εelastic
26
what is stainless steel made of
iron and chromium
27
minimum size of weld based on size of thicker plate
``` thicker plate min size of weld <10 mm 3mm 11 ~ 20 mm 5mm 21~32 mm 6mm >32mm 8mm ```
28
maximum size of weld
T - 1.5mm | 0.75 T
29
reasons of flange buckling, web buckling, web crippling
Flange buckling - Bending compression Web buckling - Diagonal compression web crippling - Bearing stress
30
permissible deflections in gantry girder
span/500 manual operated span/750 electrically operated span/1000 capacity > 50t
31
use criteria of stiffners in Plate girders
d1/tw >90, verticle stiffners for web buckling d1/tw > 200, horizontal stiffners at 0.2d from flange d1/tw > 250, horizontal at N.A d1/tw > 400, section redesign
32
end bearing stiffners Leff, area
Leff = 0.7*L1 A = 4*Aoutstand + 40*tw*tw designed as columns so tight bearing
33
outstand Area of outstand leg
A2e= k*A2 k = 3*A1 /(3A1+A2) Ae = A1 + k*A2 , 0.875A in case of symmetric angle
34
for field rivets , permissible stresses are reduced by what percentage?
10%
35
The critical slope of a roof truss above which snow load need not be considered.
50 degree
36
slenderness ratio of bracing for hangers
160
37
if beams arent restrained by cleats at ends for torsion
Length increased by 20%
38
design wind speed factors k1, k2, k3
``` k1 = risk cofficient k2 = terrain, height , size factor k3 = topography factor ```
39
The depth of web of a plate girder usually varies between
1/8 to 1/12 of the span.
40
From serviceability requirement the web is considered to be unstiffened if the spacing of transverse stiffeners is greater than
3 times the web depth.
41
batten design properties
Column is divided into a minimum of three bays (i.e. minimum 4 number of battens required). - Thickness of batten plate shall not be less than 1/50th the distance between outer most connecting line of rivets of welds. ``` - (i) Effective depth of intermediate battens > 0.75 α > 2 *b*g {b = width of column component α= spacing of C.G. of column} ``` (ii) Effective depth of end battens > α > 2*b
42
approximate are of web and flange contributing in strength of plate girder
Aeff = Aflange + (1/6)*Aweb
43
maximum spacing of purlins in asbestos roofing
1.4 m
44
Max Moment in continuous members like purlin
w.L^2 /10
45
Effective length of compression flanges depending on end conditions
Effective length of compression flanges depending on end conditions ends of compression flange unrestrained = L ends of compression flange partially restrained = 0.85L ends of compression flange fully restrained = 0.7 L cantilevers -built in support, free at end = 0.85L -built in support, restrained against torsion at end by continuous construction = 0.75L -built in support, restrained against torsion at end by cross members over several beams = 0.5L - continuous and unrestrained against torsion at support and free at end = 3L - continuous and partially restrained against torsion at support and free at end = 2L continuous and restrained against torsion at support and free at end = L