Synthesis of design and construction practices



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[123doc] - phat-trien-nguon-nhan-luc-cua-cong-ty-co-phan-misa-doc
Fatigue Cracking.  In order to model the fatigue cracking distress two approaches were 

taken: (1) model the number of load repetitions to fatigue failure of the HMA layer, and (2) 

model the number of load repetitions to fatigue failure of the rigid base layer.   

 

The modeling of fatigue failure of the HMA layer was based on the model presented by 



the proposed MEPDG (NCHRP 1-37A), which is based on the Asphalt Institute fatigue model. 

 

 



3.291

0.854


'

f

1



t

1

1



N

0.00432 k

C

E

⎛ ⎞



⎛ ⎞

=

× × ⎜ ⎟



⎜ ⎟

ε

⎝ ⎠



⎝ ⎠

(11)


 

M

C 10



=

 

(12)



 

b

a



b

V

M 4.84



0.69

V

V



=





+



 

(13)


 

where 


 

 

N



f

 = number of load repetitions to fatigue cracking 

 

'

1



k

 = parameter used for either bottom-up or top-down criteria 

 

ε

t



 = tensile strain at critical location 

 

E = stiffness of material (HMA) 



 

V

b



 = effective binder content (%) 

 

V



a

 = air voids (%) 

 

For bottom-up cracking, the 



'

1

k



 parameter is: 

 

 



(

)

ac



'

1

11.02 3.49 h



1

k

0.003602



0.000398

1 e


×

=



+

+

(14)



 

 



 18

where 


 

h

ac



 = total thickness of asphalt layer (in). 

 

In the rigid layer fatigue case, the modeling was based on two criteria: (1) the MEPDG 



CSM fatigue failure transfer function for soil cement, CTB, and lean mix (Equation 15) and (2) 

the PCA concrete fatigue failure transfer function for RCC and PCC (Equations 16 through 19). 

 

 

( )



t

c1

f



c2

0.972


MR

log N


0.0825



σ



β − ⎜





=



β

(15)


 

where 


 

 

N



f

 = number of repetitions to fatigue cracking of the CSM layer 

 

σ

t



 = maximum traffic-induced tensile stress at the bottom of the CSM layer (psi) 

 

MR = 28-day modulus of rupture (flexural strength) (psi) 



 

c1

c2



,

β β  = field calibration factors; the default factor of 1 was used for this study. 

 

SR ≥ 0.55: 



( )

f

Log N



11.737 12.077 SR

=



×

(16)


0.45 < SR < 0.55: 

3.268


f

4.2577


N

SR 0.4325



= ⎜





 

(17)



SR ≤ 0.45: 

N

f



 = unlimited 

(18)


 

where 


 

 

SR = ratio of equivalent stress to PCC flexural strength (as defined in Eq. 19) 



 

N

f



 = allowable number of repetitions to fatigue cracking. 

 

 



eq

SR

MR



σ

=

 



(19)

 

where 



 

 

eq



σ

= equivalent stress = flexural stress in slab 

 

MR = modulus of rupture of concrete = PCC flexural strength. 



 


 19

Permanent Deformation (Rutting) Modeling.  

The modeling of rutting in the HMA 

layer uses the relationship from the MEPDG (NCHRP, 2004), Equation 20, to obtain the 

accumulated plastic strain.  This strain results from the sum of various plastic strain deformations 

inside the bituminous layer, which can be used to determine the rut depth after a specific number 

of load repetitions.  To compute the rut depth, the HMA layer is divided into sub-layers 

according to the criterion described in the MEDPG, and plastic strains are computed at various 

points located at different depths from the surface.   

 

 

p



3.4488

1.5606


0.479244

1

r



k 10

T

N



ε

= ×



×

×

ε



(20)

 

where 



 

 

ε



p

 = accumulated plastic strain at N repetitions of load (in/in) 

ε

r

 = resilient strain of the asphalt material as a function of mix properties, temperature, 



and time rate of loading (in/in) 

 

N = number of load repetitions 



 

T = temperature (°F) 

 

k

1



 = parameter computed from Equation (21). 

 

 



(

)

depth



1

1

2



k

C

C



depth

0.328196


=

+

×



×

 

(21)



 

2

1



ac

ac

C



0.1039 h

2.4868 h


17.342

= −


×

+

×



(22)


 

2

2



ac

ac

C



0.0172 h

1.7331 h


27.428

=

×



×

+



 

(23)


 

where 


 

 

k



1

 = confining pressure correction factor 

 

h

ac



 = total asphalt layers thickness (in) 

 

depth = depth to computational point (in). 



 

 


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