Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness)...
-
date post
15-Jan-2016 -
Category
Documents
-
view
219 -
download
0
Transcript of Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness)...
![Page 1: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/1.jpg)
Approaches to Design
![Page 2: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/2.jpg)
Past Design Practice• Fatigue Based – (Equations)
• Serviceability (roughness) Based
• Systems Approach
![Page 3: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/3.jpg)
Design Components
• Slab length, thickness, and width
• Concrete strength
• Base/subbase materials
• Joint type
• Subdrainage
• Shoulder type
• Use of reinforcement
![Page 4: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/4.jpg)
Empirical Approach
INPUTS
• SLAB h• K-VALUE• ESAL• PCC M.R.
STATISTICAL
REGRESSION
MODEL
OUTPUTS• PSI
![Page 5: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/5.jpg)
Mechanistic Approach
INPUTS
• SLAB h• K-VALUE• AXLE LOAD & VOL.• PCC M.R.
SLAB
STRESS
MODEL
σ
FATIGUE
DAMAGE
MODEL
n
N
CALIBRATION
WITH SLAB
CRACKING
OUTPUTS
• CRACKING
![Page 6: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/6.jpg)
Components of PCC Mechanistic Design
Design Inputs
-Material Properties K value Modulus of rupture E Value-Traffic level and distribution-Climatic factors
Design Options
-Subbase-Shoulder-Joint type and spacing-Service level Cracking level Design reliability
-Select Trial Thickness-Axle load curves and stresses-Curling Stress
Structural Model
-Traffic distribution-Allowable application
Fatigue Damage Analysis
-Fatigue Damage vs. performance
Evaluate Design
Final DesignDesign Iterations
![Page 7: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/7.jpg)
DowelBar
Subgrade
Critical Stress forMid Slab Loading
SlabThickness
Slab Length (L)
Single Axle Loading
Agg
Subbase
he
w
s
a
Traffi
c Lan
e
Should
erH
inge
Join
t
Hin
ge Jo
int
Do
3
4 2
Eh=
12 1- k
![Page 8: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/8.jpg)
Finite Element Slab Layout for Single Axle Load.
12”
15”
Wheel Load
Typical Element
Typical Nodal Point
15’
12’
30” 24” 24” 12” 12” 24” 24” 30”
12”
24”
24”
24”
24”
24”
12”
![Page 9: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/9.jpg)
Loading Conditions for Westergaard Equations
2 21e 2 2
a a6Pσ 0.489log 0.091 0.027h
(b)
(a)e 2 2
3P1 ν 1 3P1 ν2σ ln γ2π 2 2πh ha
(c)'6
1c 2
a3Pσ = 1-h
a2a
a 1
2e
σ hs= Dimensional stressP
![Page 10: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/10.jpg)
Medium Thick Plate Equation
![Page 11: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/11.jpg)
Z
X
Y
x
yz
zx zy
y
xz
y
x
xy
z
Notation & SignConvention
Stress Element – Medium Thick Plate
![Page 12: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/12.jpg)
Elastic, Homogenous, “Medium - Thick Plate”
A. Thickness = 1/20 to 1/100 of L
B. Plate can carry transverse loads by flexure rather than in-plane force (thin membrane) but not so thick that transverse shear deformation becomes important.
C. Deformations are small - such that in-plane forces produced by stretching of the middle surface are negligible.
D. To reduce the three-dimensional stress analysis problem to two-dimensions, two basic assumptions:
![Page 13: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/13.jpg)
1. Applied stress on the boundary faces of the plate are small compared to other stresses in the plate. Direct stresses in the thickness direction is negligible.
0
&0
0
,,
yz
xyyxxz
z
Plane Stress Condition:
Specifies the state of stress
![Page 14: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/14.jpg)
2. A line normal to the middle surface before deformation remains normal and unstretched after deformation. (Similar to Bernoulli assumption in engineering beam theory):
vv yxz
yxz
yzxzz
)(
&
0
Plane Strain Condition:
Is found in terms of
Poisson’s Ratio
![Page 15: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/15.jpg)
h
y zy
dzdx
xy
Stress Acting on a lamina of thickness dz at a distance of z from themiddle surface
yx
x
x
dy
0
0Z
z xz yz
F
![Page 16: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/16.jpg)
Assumptions: classical “medium-thick plate” theory
1. All forces on the surface of the plate are perpendicular to the surface (i.e. no shear or frictional forces).
2. The slab is of uniform cross-section (i.e. constant thickness).
3. In-plane forces do not exist (i.e. no membrane forces).
4. X-Y plane (neutral axis) is located mid-depth within the slab (i.e. stresses and strains are zero at mid-depth).
![Page 17: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/17.jpg)
5. Deformation within an elemental volume which is normal to the slab surfaces can be ignored (i.e. plane strain ).
6. Shear deformations are small and are ignored; shear forces are not ignored.
7. Slab dimensions are infinite. However empirical guidelines have been developed for the least slab dimension L, required to achieve the infinite slab condition.
8. Slab on a Winkler foundation-subgrade is represented as discrete springs beneath the slab.
0z
![Page 18: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/18.jpg)
E. The stress resultants are defined in terms of the stresses: (per unit length of mid surface)
In Plane Stress
2
2
2
2
2
2
0
0
0
h
h
xyxy
h
h
yy
h
h
xx
dzN
dzN
dxN
Normal force per unit width - No membrane forces
![Page 19: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/19.jpg)
Transverse Shears:
2
2
2
2
0
0
h
x xzh
h
y yzh
V dz
V dz
Force/Unit Length
NOTE: The transverse shears are determinedby statics. They cannot be determined fromthe stress - strain relations since we have assumed xz = yz = 0. This is the samesituation as exists in beam theory. The transverse shears are necessary for equilibriumeven though the strains associated with themhave been assumed to be zero.
![Page 20: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/20.jpg)
Sign Convention for Stress
Resultants
x
Mx
Nx
Vx
Nxy
Mxy
Nyx
MyxMy
Ny
Vyz
Y
![Page 21: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/21.jpg)
Bending Moments per unit length
2
2
2
2
2
2
h
h
xyxy
h
h
yy
h
h
xx
dzzM
dzzM
dzzM
(Positive when compression occurs on top of slab)
Twisting moment
![Page 22: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/22.jpg)
![Page 23: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/23.jpg)
Equilibrium Equations
0
0
0
02 2
Z
yxx x y y
yx
y
yxxx x yx yx
xx x
F
VVpdxdy V dy V dx dy V dx V dy dx
x y
VVp
x y
M
MMM dy M dx dy M dx M dy dx
x y
V dx dxV dx dy V dy
x
![Page 24: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/24.jpg)
02
Using 0
yxxx
yxxx
x
y xyy
MM Vx dxdxdy dxdy dxdy V dxdy
x y x
MMV
x y
M
M MV
y x
Second order term = 0
(2)
(3)
![Page 25: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/25.jpg)
Substituting equation 2 & 3 into equation 1 gives:
pyx
M
y
M
yx
M
x
M xyyxyx
2
2
22
2
2
Based on statics; no material properties
for beams all
*NOTE: BEAMS
py
M
yx
M
x
M yxyx
2
22
2
2 2
0y
pdx
Md
2
2 dVp
dx
dMV
dx
![Page 26: Approaches to Design. Past Design Practice Fatigue Based – (Equations) Serviceability (roughness) Based Systems Approach.](https://reader036.fdocuments.in/reader036/viewer/2022062518/56649d4a5503460f94a26de2/html5/thumbnails/26.jpg)
M may be statically determinate - depending on the boundaryconditions. The plate is intrinsically indeterminate since there are 3 moment Mx, My, and Mxy and 1 equation of statics; to proceed further, consideration of deformations is required.