Title: Two-Span LRFD Design Example
1Two-Span LRFD Design Example
- Karl Barth and Jennifer Righman
- West Virginia University
2Objective
- The primary focus of this example
- is to demonstrate the use of
- Appendix A and Appendix B
- for a two-span continuous structure
3Appendix A Overview
- Accounts for the ability of compact and
non-compact sections to resist moments greater
than My - Economy gained by Appendix A provisions increases
with decreasing web slenderness - Effects of St. Venant torsion are incorporated
4Appendix B Overview
- Traditional AASHTO specifications have permitted
up to 10 of the maximum pier section bending
moment to be redistributed to positive bending
regions - Appendix B provisions explicitly compute the
level of redistribution based on an effective
plastic moment concept for sections meeting
prescribed geometric criteria
5Design Information
6Design Information
7Design Notes
- 2004 AASHTO LRFD Specifications, 3rd Edition
- Structural steel ASTM A709, Grade 50W
- Normal weight concrete (145 pcf) with fc4 ksi
- Fyr 60 ksi for reinforcing steel
- Operational importance, redundancy, and ductility
factors 1.0
8Design Loads DC1
- DC1 loads are equally distributed to all girders
- Slab 0.983 k/ft
- Haunch (average wt/length) 0.017 k/ft
- Overhang taper 0.019 k/ft
- Girder (average wt/length, varies) 0.200 k/ft
- Cross-frames and misc. steel 0.015 k/ft
- Stay-in-place forms 0.101 k/ft
- S 1.335 k/ft
-
9Design Loads DC2 and DW
- DC2
- Barrier weight 520 lb/ft
- Weight/girder (0.520)x(2)/(4) 0.260 k/ft
- DW
- Future wearing surface 25 psf
- DW (0.025 ksf)x(34 ft)/4 0.213 k/ft
10Design Loads WS and WL
- WS
- Wind forces are calculated assuming bridge is
located 30 above water in open country - Wind on upper half of girder, deck, and barrier
assumed to be resisted by diaphragm action of the
deck - WS 0.081 k/ft (on bottom flange)
- WL
- Assumed to be transmitted by diaphragm action
- WL is neglected
11Design Loads Live Load
- Controlling case of
- Truck Lane
- Tandem Lane
- 0.9 (Double Truck Lane) (in negative bending)
- Impact factors used for all vehicular live loads
(excluding lane load) - I1.15 for fatigue limit state
- I1.33 for all other limit states
12Design Loads Live Load
- Live load effects are approximated using
distribution factors - Interior girder
- AASHTO empirical equations are used
- Exterior girder
- AASHTO empirical equation correction factor
- Lever rule
- Special analysis
13Interior Girder Distribution Factors
- Moment
- Varies with girder dimensions due to Kg term
- One design lane
- Two or more design lanes
14Interior Girder Distribution Factors
- Shear
- One design lane
- Two or more design lanes (CONTROLS)
15Exterior Girder Distribution Factors
- AASHTO exterior girder correction factor
- Moment
- Shear
- Empirical formulas for exterior girder will not
control
16Exterior Girder Distribution Factor
- Lever Rule One Design Lane
17Exterior Girder Distribution Factor
- Special Analysis
- One design lane
- Two or more design lanes
18Distribution Factors for Fatigue
- Based on one design lane
- No multiple presence factor applied
- Maximum one lane distribution factor results from
the lever rule, i.e., EXTERIOR GIRDER CONTROLS - DF 0.70
19Unfactored Design Moments
20Limit States
- All applicable limits states for steel structures
were considered - Strength
- Strength I controls in this example
- Strength I 1.25DC 1.5DW 1.75(LLI)
- Strength III 1.25DC 1.5DW 1.4WS
- Strength IV 1.5(DC DW)
- Strength V 1.25DC 1.5DW 1.35(LLI) 0.4WS
- Service
- Service II 1.0(DC DW) 1.3(LLI)
- Fatigue 0.75(LLI)
216.10 Provisions Addressed
- Cross section proportion limits
- Constructibility
- Serviceability
- Fatigue
- Strength
22Appendix A Design
23Cross Section Proportion Limits
24Constructibility
- For discretely braced compression flanges
- Fnc may be computed using Appendix A which
accounts for increased torsional resistance - For discretely braced tension flanges and
continuously braced flanges
25Constructibility - Loads
- Vertical DC1 loads are determined considering
deck casting sequence - Lateral flange bending stresses
- are induced by the overhang form brackets
- Construction dead and live loads considered
26Constructibility Check
- Stresses in compression flange of positive
bending section control the allowable cross-frame
spacing - Strength I
- Strength IV
27Service Limit State
- For top flange
- For bottom flange
- Bottom flange in positive bending (controls)
28Fatigue Limit State
- Fatigue requirements significantly impact the
design of the positive bending region - Bolted stiffener to flange connections employed
at locations of maximum stress range, i.e.,
cross-frames at midspan - Bolted connections / Category B details
- Welded connections / Category C details
29Fatigue Limit State (cont.)
- Use of bolted cross-frame connections requires
that net section fracture requirements are
satisfied - Assuming one 7/8 diameter bolt hole is used
30Positive Flexural Capacity
- If , then
- Otherwise
- Unless certain geometric conditions are satisfied
-
- Ductility check
31Negative Flexural Capacity Appendix A
-
-
- Therefore, Appendix A is applicable.
32Web Plastification Factors
- Check if web is compact - NO
- Noncompact web plastification factors are used
33Web Plastification Factors (cont.)
34Compression Flange Local Buckling Resistance
- Check if flange is compact - YES
-
35Lateral Torsional Buckling Resistance
36Lateral Torsional Buckling Resistance
37Negative Flexural Capacity Summary
38Appendix A Performance Ratios Positive Bending
Region
Constructibility (Strength I) Top Flange 0.94
Constructibility (Strength I) Bottom Flange 0.30
Constructibility (Strength IV) Top Flange 0.93
Constructibility (Strength IV) Bottom Flange 0.36
Service Limit State Top Flange 0.47
Service Limit State Bottom Flange 0.70
Fatigue and Fracture Limit State Bolted Conn. 0.80
Fatigue and Fracture Limit State Welded Conn. 0.98
Strength Limit State (Strength I) Flexure 0.69
Strength Limit State (Strength I) Shear 0.83
39Appendix A Performance Ratios Negative Bending
Region
Constructibility (Strength I) Top Flange 0.46
Constructibility (Strength I) Bottom Flange 0.34
Constructibility (Strength IV) Top Flange 0.55
Constructibility (Strength IV) Bottom Flange 0.39
Service Limit State Top Flange 0.57
Service Limit State Bottom Flange 0.69
Fatigue and Fracture Limit State Bolted Conn. NA
Fatigue and Fracture Limit State Welded Conn. 0.58
Strength Limit State (Strength I) Flexure 0.96
Strength Limit State (Strength I) Shear 0.78
40Appendix B Design
- Moment redistribution procedures are used to
create a more economical design
41Appendix B Requirements
- Appendix B is valid for girders meeting certain
geometric and material limits - Web Proportions
-
-
-
-
42Appendix B Requirements (cont.)
- Compression flange proportions
-
-
-
- Lateral Bracing
-
-
43Appendix B Requirements (cont.)
- Shear
-
- Section Transitions
- No section transitions are permitted within the
first cross-frame spacing on each side of the
pier -
- Bearing Stiffeners
- Bearing stiffeners are required to meet
projecting width, bearing resistance, and axial
resistance requirements -
44Redistribution Moment
- Amount of moment redistributed to positive
bending region is a function of the effective
plastic moment, Mpe - Higher Mpe values are permitted for girders with
either - Transverse stiffeners placed at D/2 or less on
each side of the pier - Ultra-compact webs such that
- Alternative Mpe equations are given for strength
and service limit states -
-
45Redistribution Moment (cont.)
-
-
- Redistribution moment at pier
-
- Redistribution moment
- varies linearly at other
- locations along the span
46Redistribution Moments (Strength I)
47Appendix B Design Checks
- Positive bending capacity
- Evaluated for positive bending moment plus
redistribution moment (at strength and service
limit states) - Negative bending capacity within one lateral
brace spacing on each side of the pier - Not evaluated
- Negative bending capacity at other locations
- Evaluated for negative bending moment minus
redistribution moment - Otherwise, same as before
48Appendix B Performance Ratios Positive Bending
Region
Constructibility (Strength I) Top Flange 0.94
Constructibility (Strength I) Bottom Flange 0.30
Constructibility (Strength IV) Top Flange 0.93
Constructibility (Strength IV) Bottom Flange 0.36
Service Limit State Top Flange 0.47
Service Limit State Bottom Flange 0.70
Fatigue and Fracture Limit State Bolted Conn. 0.80
Fatigue and Fracture Limit State Welded Conn. 0.99
Strength Limit State (Strength I) Flexure 0.75
Strength Limit State (Strength I) Shear 0.83
49Appendix B Performance Ratios Negative Bending
Region
Constructibility (Strength I) Top Flange 0.55
Constructibility (Strength I) Bottom Flange 0.42
Constructibility (Strength IV) Top Flange 0.66
Constructibility (Strength IV) Bottom Flange 0.48
Service Limit State Top Flange 0.62
Service Limit State Bottom Flange 0.79
Fatigue Limit State Welded Conn. 0.55
Strength Limit State (Strength I) Flexure 0.48
Strength Limit State (Strength I) Shear 0.78
Design of negative bending region controlled by
20 limit
50Appendix A / Appendix B Design Comparisons
- Positive moment region same in both designs
(controlled by fatigue) - Cross-frame spacing the same
- (controlled by constructibility)
- Appendix B negative moment region 18 lighter
- Appendix B girder 6 lighter overall
51Concluding Comments
- Fatigue requirements significantly impact the
design of the positive moment region due to the
relatively high distribution factor for the
exterior girder - Constructibility and Appendix B requirements led
to the use of a 15 ft cross-frame spacing
throughout - Use of Appendix A leads to increasing economy
with decreasing web slenderness (that is a
section with a noncompact web at the upper limit
will gain very little from Appendix A) - Appendix B provides even greater economy
52QUESTIONS?