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Giải thích hệ số PBN - Kennedy and Sennah

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Tiêu đề Giải thích hệ số PBN - Kennedy and Sennah
Tác giả Kennedy And Sennah
Trường học Bridgetech, Inc.
Thể loại Bài luận
Định dạng
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Task 2 – Range of structural forms, materialsand range of application  There is no reason at this point to limit range of application we can include range outside of conventional practi

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Kennedy and Sennah

better accuracy)

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European Practice

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Summary

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Task 2 – Range of structural forms, materials

and range of application

 There is no reason at this point to limit range of

application (we can include range outside of

conventional practice and geometries)

 “All” parameters will be included in the

database

 A large amount of data is available from

several sources (see Task 6 tables)

 Additional data can be added

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Task 3 Analytical method

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Task 3 Analytical method

Numerical methods

 Finite difference

 Finite element method (plate or shell elements)

 Grillage

 Finite Strip Method

 Harmonic analysis (Sanders and Elleby)

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Theorem Requirements

forces are in equilibrium

must be ductile

Independent of themodeling assumptions!

No instability or fracture

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The lower bound theorem is one of the most important

theorems/concepts in

structural engineering.

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The lower bound theorem is

one of the most important

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Task 4 Process Detail and Chaining

Effort Do it? Sample

1 12-50 -> BRASS -> Computation -> 12-50 Small yes

2 12-50 -> BRASS -> Input File -> FEA -> 12-50 Large yes

3 12-50 -> BRASS -> Input File -> FSM -> 12-50 Medium yes

Process NCHRP 12-50

CSA NCHRP 12-62

TN Tech, Set 1

12-26

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Task 4 Process Matrix

Notes NCHRP 12-50 TN Tech Set 1 NCHRP 12-26 CSA Sanders LRFR AASHTO Std S/D equation, program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

AASHTO LRFD LRFD Eqs, program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

AASHTO LRFD Lever Rule Program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

AASHTO LRFD Rigid Method Program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

Sanders Program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

Canadian Specification (CSA) Program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

Henry (Modified) Program into an automated approach process 1 process 4 process 7 process 10 process 13 process 16

Rigorous FEA FEA engine and/or a commercial FEA engine process 2 process 5 process 8 process 11 process 14 process 17

Rigorous FSM Available FSM program process 3 process 6 process 9 process 12 process 15 process 18

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Task 6 – Parametric Study

 321 Total Data Sets

 AASHTO Type A

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Task 6 – Parametric Study

 176 Total Data Sets

 AASHTO Type K

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Task 6 – Parametric Study

 74 Total Data Sets

 AASHTO Types E and J

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Task 6 – Parametric Study

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Task 6 – Parametric Study

 Spread Concrete Boxes

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Task 6 – Parametric Study

 307 Total Data Sets

 AASHTO Types D, F, and G

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Task 6 Wood Bridges

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Additional Load Distribution Issues

Parameters Skew Barriers Diaphragms Location

Location (e.g Fatigue) Maybe Yes Maybe Yes

Additional Parameters

Perform separate parametric studies to focus

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Three primary questions for the

panel

lanes

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Number of Lanes Loaded

•Issue for our study – not total design load for girder systems

•Integer number

or decimal value

•Should not be overly sensitive to

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Live Load Position – Interior Girder

6-4-6-6 (critical)

6-4-6-4-6 (critical)

6-6-6-6-6 (critical)

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Live Load Position (exterior girder)

2-6-4-6-6

2-6-4-6-4-6

2-6-6-6-6-6

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Multiple Presence – separate from

live load distribution

 Task 6 distribution factors will be computed for

one-, two-, three-, etc-lanes loaded This could be

combined, if necessary, later

Research simplified methods will not include m.

 Rearch simplified methods will permit one-, two-,

three-, etc-lanes loaded to be computed and

independently applied

 The specification can clearly indicate (apriori)

how the number of controlling lanes, i.e., it can be

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0.851.01.2

MultiplePresenceFactor

z.Z3

y.Y2

x.X1

FactorRequired byMethod

Number of

lanes loaded

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