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SDA-08-001 Gusset Plate Design

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    New York State Department of Transportation

    OFFICE OF STRUCTURES

    STRUCTURES DESIGN ADVISORYIssued by:MAIN OFFICE,OFFICE OFSTRUCTURES

    SUBJECT:

    GUSSET PLATES DESIGNPROCESS

    CODE:SDA 08-001

    DATE:14 Apr 2008

    APPROVED BY: SUBJECT CODE: SUPERSEDES:NONE

    PURPOSE

    AASHTOs Standard Specifications for Highway Bridges and the Load and Resistance Factor Design(LRFD) Specifications do not prescribe hard and fast methods for gusset plate design. Rather, generalengineering principles and textbook methods are used for gusset plate design. This Design Advisory willprovide additional guidance, including an example, to designers of new or replaced non-load-path-

    redundant steel truss bridges.

    BACKGROUND

    On August 1, 2007, the I-35W Interstate highway bridge over the Mississippi River in Minneapolis,Minnesota, experienced a failure in the superstructure of the steel deck truss. Physical examination of therecovered bridge structure showed that some gusset plates were fractured. Examination of the designmethodology used at the time was found to be sound. Although no problems were identified with thedesign methodology used for the bridge, the investigation discovered that some gusset plates on the maintrusses of the bridge were undersized.

    Accordingly, NYSDOT put in place an implementation plan to address FHWA recommendations regardingLoad-carrying Capacity Considerations of Gusset Plates in Non-load path redundant Steel TrussBridges. On January 15, 2008 FHWA issued a Technical Advisory that made three recommendationscovering: new or replaced non-load-path-redundant steel truss bridges, future recalculations of loadcapacity on existing non-load-path-redundant steel truss bridges, and reviewing previous load ratings ofgusset plates on bridges subjected to significant changes in stress levels. This Structures Design

    Advisory (SDA) addresses new or replaced non-load-path-redundant steel truss bridges.

    A separate NYSDOT Load Rating Technical Advisory is being issued to address the otherrecommendations.

    TRUSS GUSSET PLATE DESIGN AND ANALYSIS

    Ordinarily, gusset plates are stronger than the truss members they connect and should not control thecapacity of the structure. There are several possible approaches to the design and analysis of truss gussetplates. A recommended procedure is outlined in this Structures Design Advisory (SDA). Other analysis

    procedures may be used if they are soundly documented and considered to be applicable for the bridgeunder design.

    The gusset plate design shall be made using AASHTOs Load and Resistance Factor Design (LRFD)Specifications with the HL-93 and NYSDOT Design Permit Vehicle for Live loads.

    Truss member connections shall be designed at the strength limit state for not less than the larger of theaverage of the axial force due to the factored loadings at the point of splice or connection and the factoredaxial resistance of the member at the same point OR 75 percent of the factored axial resistance of themember per LRFD Article 6.13.1. The aforementioned LRFD article does not apply to sections ofinterest.

    The maximum stress on a section due to the factored loads shall be checked in accordance with LRFDArticle 6.14.2.8.

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    STRUCTURES DESIGN ADVISORYCODE:

    DATE: 14 Apr il 2008 PAGE: 2

    SUBJECT:GUSSET PLATES DESIGN PROCESS

    LIVE LOAD CASES

    Four live load cases will be considered at each truss joint:

    1. Position the HL-93 live load plus impact such that the factored force in the higher loaded chord ismaximized while using the corresponding forces for that case in the diagonals and verticals at that

    joint.

    2. Position the HL-93 live load plus impact such that the factored force in the higher loaded diagonalis maximized while using the corresponding forces for that case in the chords and vertical at that

    joint.

    3. Position the NYSDOT Design Permit Vehicle live load plus impact such that the factored force inthe higher loaded chord is maximized while using the corresponding forces for that case in thediagonals and verticals at that joint.

    4. Position the NYSDOT Design Permit Vehicle live load plus impact such that the factored force inthe higher loaded diagonal is maximized while using the corresponding forces for that case in thechords and vertical at that joint.

    SECTIONS OF INTEREST

    At least four sections, two horizontal sections located adjacent to the chord and two vertical sectionslocated on either side of the vertical member, shall be investigated at each truss joint. These sections areillustrated in the attached Math Cad worksheet. An additional section shall also be investigated at truss

    joints where there is a break in the alignment of the chord. Additional sections should be investigated atunusual truss joint configurations.

    At each of these sections the following are to be checked:

    Maximum stress from combined factored flexural and axial loads on thegross and net sections.

    Uniform and maximum shear stress on both the gross and net sections.

    UNSUPPORTED EDGE DISTANCE

    The unsupported edge distance of gusset plates should be designed in accordance with LRFD Article6.14.2.8

    EDGE SLENDERNESS RATIO REQUIREMENT

    The edge slenderness of gusset plates should be designed in accordance with LRFD Article 6.9.3

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    STRUCTURES DESIGN ADVISORYCODE:

    DATE: 14 Apr il 2008 PAGE: 3

    SUBJECT:GUSSET PLATES DESIGN PROCESS

    MEMBER CONNECTION FORCE

    Four cases will be considered at each member:

    1. Maximum tensile force in the member due to dead load plus HL-93 live load plus impact.

    2. Maximum compressive force in the member due to dead load plus HL-93 live load plus impact.

    3. Maximum tensile force in the member due to dead load plus NYSDOT Design Permit Vehicle liveload plus impact.

    4. Maximum compressive force in the member due to dead load plus NYSDOT Design PermitVehicle live load plus impact.

    BOLT CAPACITY

    The capacity of the bolts connecting the truss members to the gusset plates shall be designed for themaximum truss member force and in accordance with LRFD Articles 6.13.1 & 6.13.2.

    BLOCK SHEAR RUPTURE RESISTANCEGusset plates should be designed for block shear rupture in accordance with LRFD Article 6.13.4.The analysis of block shear rupture involves the evaluation of several patterns of planes to arrive at thegoverning pattern.

    ANALYSIS OF WHITMORE SECTION

    The tensile stress on the gusset plate shall also be checked at the Whitmore Section. This considers the

    axial load applied to the gusset plate individually by each truss member to the Whitmore Section.

    The Whitmore Section is defined in the attached Math Cad worksheet.

    BUCKLING CHECK OF COLUMN UNDER COMPRESSION MEMBERS

    The resistance of gusset plates in compression shall be determined as that of idealized members incompression in accordance with the provisions of AASHTO LRFD Articles 6.9.2.1 and 6.9.4.

    WORKED EXAMPLE

    An example using a Math Cad worksheet is distributed along with this Structures Design Advisory.

    CONTACT:

    Direct questions regarding this SDA to Wahid Albert of the Structures Design Bureau at (518) 457 4539,or by e-mail to [email protected]

    mailto:[email protected]:[email protected]
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    STRUCTURES DESIGN ADVISORYCODE:

    DATE: 14 Apr il 2008 PAGE: 4

    SUBJECT:GUSSET PLATES DESIGN PROCESS

    REFERENCES

    National Transportation Safety Board Safety Recommendation H-08-1, dated January 15, 2008.

    FHWA Technical Advisory T 5140.29, Load Carrying Capacity Consideration of Gusset Plates inNon-Load-Path Redundant Steel Truss Bridges, dated January 15, 2008.

    FHWA Bridge Design Guidance No. 1, Revision Date of February 28, 2008.

    AASHTO LRFD Bridge Design Specifications, 4thEdition/2007, " Washington, DC, 2004.

    AISCs Manual of Steel Construction, Load and Resistance Factor Design, Third Edition, Part 9,Dated November 2001.

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 1 of 77PIN: ________

    Job Title: ____________________

    This Mathcad worksheet is intended to analyze gusset plates according to the AASHTO LRFD Bridge Design

    Specifications, 4th Edition 2007. Gusset plates are analyzed for shear, bending, and axial force effects by theconventional "Method-of-Section" procedures. It should be noted that this sheet only investigates three common

    sections of interest, two vertical and one horizontal section. Additional sections should be investigated at joints

    that have a break in the alignment of the chord and/or unusual joint configurations. Member connections are

    analyzed for bolt resistance, block shear rupture resistance, and Whitmore section stresses.

    Disclaimer: This worksheet and sample calculations outline an acceptable method for designing truss gusset

    plates. There may be other acceptable procedures for this design. While this Mathcad sheet has been checked,

    it should be used by an engineer familiar with truss and gusset plate design. Sound engineering judgement is

    required to apply this method to individual situations and to bridges that may vary from this example.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 2 of 77PIN: ________

    Job Title: ____________________

    Member Angles and Unsupported Edge Distances

    A 90 deg

    B 42.5 deg

    C 0deg

    D 40.2deg

    E 90deg

    B1 31.0in

    B2 28.0in

    B3 25.0in

    B4 31.4in

    Angle from Vertical: Input a positive angle for members that are clockwise from vertical and a negative angle for

    members that are counter clockwise from vertical.

    Unsupported Edge Distances: The unsupported edge distances of the top and side of the gusset plate should

    be taken from the center to center of the outermost bolt holes.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 3 of 77PIN: ________

    Job Title: ____________________

    Unfactored Member Forces Due to Dead Load

    Dead Load (DC) Dead Load (DW)

    Member A ADC 1779kip ADW 103kip

    Member B BDC 266kip BDW 15kip Tensile +Compressive -

    Member C CDC 25 kip CDW 0kip

    Member D DDC 5 kip DDW 0kip

    Member E EDC 1940kip EDW 109kip

    Dead Load (DC): Enter the unfactored member force due to dead load. Input tensile force as a positive value and

    compressive force as a negative value.

    Dead Load (DW): Enter the unfactored member force due to future wearing surface and utilities. Input tensile

    force as a positive value and compressive force as a negative value.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 4 of 77PIN: ________

    Job Title: ____________________

    Unfactored Member Forces Due to HL-93 Live Load + Impact

    Case 1 Case 2

    Member A AHL1 415kip AHL2 345kip

    Member B BHL1 110kip BHL2 142kip

    Tensile +

    Compressive -Member C CHL1 2kip CHL2 3kip

    Member D DHL1 36 kip DHL2 11 kip

    Member E EHL1 521kip EHL2 434kip

    Case 1: Position the HL-93 live load such that the force in the higher loaded chord is maximized. Enter the

    unfactored chord and corresponding vertical ,diagonal, and chord member forces. Input tensile force as a positive

    value and compressive force as a negative value.

    Case 2: Position the HL-93 live load such that the force in the higher loaded diagonal is maximized. Enter the

    unfactored diagonal and corresponding vertical, diagonal, and chord member forces. Input tensile force as a

    positive value and compressive force as a negative value.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 5 of 77PIN: ________

    Job Title: ____________________

    Unfactored Member Forces Due to NYSDOT Design Permit Vehicle + Impact

    (LRFD 3.6.1.2.4a Blue Page)

    Case 3 Case 4

    Member A APV3 401kip APV4 414kip

    Member B BPV3 166kip BPV4 170kip

    Tensile +Compressive -

    Member C CPV3 3kip CPV4 3kip

    Member D DPV3 55 kip DPV4 27 kip

    Member E EPV3 549kip EPV4 546kip

    Case 3: Position the permit live load such that the force in the higher loaded chord is maximized. Enter the

    unfactored chord and corresponding vertical, diagonal, and chord member forces. Input tensile force as a positive

    value and compressive force as a negative value.

    Case 4: Position the permit live load such that the force in the higher loaded diagonal is maximized. Enter the

    unfactored diagonal and corresponding vertical, diagonal, and chord member forces. Input tensile force as a

    positive value and compressive force as a negative value.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 6 of 77PIN: ________

    Job Title: ____________________

    Gusset and Splice Plate Dimensions

    tgp 1.125in

    hsp 17.3in

    t

    sp

    .75in

    Lgs 1.6in

    B 2.6in

    Yield Strength of Steel: Fy 50ksi Ultimate Strength of Steel: Fu 65ksi

    Modulus of Elasticity of Steel: E 29000ksi

    Bolt Properties

    Nominal Bolt Diameter: db 1in

    Diameter of Hole: dh 1.0625in LRFD 6.13.2.4.2-1

    Minimum Tensile Strength of Bolt: Fub 120ksi LRFD 6.4.3.1

    Minimum Required Bolt Tension: Pt 51kip LRFD 6.13.2.8-1

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 7 of 77PIN: ________

    Job Title: ____________________

    Resistance Factors

    Resistance Factor for Flexure: f 1.0 LRFD 6.5.4.2

    Resistance Factor for Shear: v 1.0 LRFD 6.5.4.2

    Resistance Factor for Tension on Gross: y .95 LRFD 6.5.4.2

    Resistance Factor for Tension on Net: u .80 LRFD 6.5.4.2

    Resistance Factor for Compression: c

    .90 LRFD 6.5.4.2

    Resistance Factor for Shear on Gross: vy .95 FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    Resistance Factor for Shear on Net: vu .80 FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    Effective Length Factor: K 1.0 LRFD 4.6.2.5

    Reduction factor for shear lag in connection: U 1.0 LRFD 6.8.2.2

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 8 of 77PIN: ________

    Job Title: ____________________

    Factored Member Forces LRFD T3.4.1-1

    Load Modifier based on ductility, redundancy, and operational importance: i 1.05 LRFD 1.3.2

    Ac1 i 1.25ADC 1.5ADW 1.75 AHL1 Ac1 3260kipAc2 i 1.25ADC 1.5ADW 1.75 AHL2 Ac2 3131kipAc3 i 1.25ADC 1.5ADW 1.35 APV3 Ac3 3066kipAc4 i 1.25ADC 1.5ADW 1.35 APV4 Ac4 3084kip

    Bc1 i 1.25BDC 1.5BDW 1.75 BHL1 Bc1 575 kipBc2 i 1.25BDC 1.5BDW 1.75 BHL2 Bc2 634 kipBc3 i 1.25BDC 1.5BDW 1.35 BPV3 Bc3 608 kipBc4 i 1.25BDC 1.5BDW 1.35 BPV4 Bc4 614 kip

    Cc1 i 1.25CDC 1.5CDW 1.75 CHL1 Cc1 29 kipCc2 i 1.25CDC 1.5CDW 1.75 CHL2 Cc2 27 kipCc3 i 1.25CDC 1.5CDW 1.35 CPV3 Cc3 29 kip

    Cc4 i 1.25CDC 1.5CDW 1.35 CPV4 Cc4 29 kip

    Dc1 i 1.25DDC 1.5DDW 1.75 DHL1 Dc1 73 kipDc2 i 1.25DDC 1.5DDW 1.75 DHL2 Dc2 27 kipDc3 i 1.25DDC 1.5DDW 1.35 DPV3 Dc3 85 kipDc4 i 1.25DDC 1.5DDW 1.35 DPV4 Dc4 45 kip

    Ec1 i 1.25EDC 1.5EDW 1.75 EHL1 Ec1 3675kipE

    c2

    i

    1.25E

    DC

    1.5E

    DW

    1.75 EHL2

    E

    c2

    3515kip

    Ec3 i 1.25EDC 1.5EDW 1.35 EPV3 Ec3 3496kipEc4 i 1.25EDC 1.5EDW 1.35 EPV4 Ec4 3492kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 9 of 77PIN: ________

    Job Title: ____________________

    Horizontal and Vertical Components of Member Forces

    Note: The applied member forces are reduced by half to account for the member being supported on both

    sides by a gusset plate.

    Member A

    FA1x .5Ac1sin A FA1x 1630 kip FA2x .5Ac2sin A FA2x 1566 kip

    FA1y .5Ac1cos A FA1y 0 kip FA2y .5Ac2cos A FA2y 0 kip

    FA3x .5Ac3sin A FA3x 1533 kip FA4x .5Ac4sin A FA4x 1542 kipFA3y .5Ac3cos A FA3y 0 kip FA4y .5Ac4cos A FA4y 0 kip

    Member B

    FB1x .5Bc1sin B FB1x 194 kip FB2x .5Bc2sin B FB2x 214 kip

    FB1y .5Bc1cos B FB1y 212 kip FB2y .5Bc2cos B FB2y 234 kip

    FB3x .5Bc3sin B FB3x 205 kip FB4x .5Bc4sin B FB4x 207 kipFB3y .5Bc3cos B FB3y 224 kip FB4y .5Bc4cos B FB4y 226 kip

    Member C

    FC1x .5Cc1sin C FC1x 0 kip FC2x .5Cc2sin C FC2x 0 kip

    FC1y .5Cc1cos C FC1y 15 kip FC2y .5Cc2cos C FC2y 14 kip

    F

    C3x

    .5C

    c3

    sin C

    FC3x

    0 kip FC4x

    .5C

    c4

    sin C

    FC4x

    0 kip

    FC3y .5Cc3cos C FC3y 14 kip FC4y .5Cc4cos C FC4y 14 kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 10 of 77PIN: ________

    Job Title: ____________________

    Member D

    FD1x .5Dc1sin D FD1x 23 kip FD2x .5Dc2sin D FD2x 9 kipFD1y .5Dc1cos D FD1y 28 kip FD2y .5Dc2cos D FD2y 10 kip

    FD3x .5Dc3sin D FD3x 27 kip FD4x .5Dc4sin D FD4x 14 kip

    FD3y .5Dc3cos D FD3y 32 kip FD4y .5Dc4cos D FD4y 17 kip

    Member E

    FE1x .5Ec1sin E FE1x 1838kip FE2x .5Ec2sin E FE2x 1758kipFE1y .5Ec1cos E FE1y 0 kip FE2y .5Ec2cos E FE2y 0 kip

    FE3x .5Ec3sin E FE3x 1748kip FE4x .5Ec4sin E FE4x 1746kip

    FE3y .5Ec3cos E FE3y 0 kip FE4y .5Ec4cos E FE4y 0 kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 11 of 77PIN: ________

    Job Title: ____________________

    Analysis of Horizontal Section A1-A1

    LAA1 90.2in

    YA1 19.618in

    XA1 46.4in

    Force Diagram

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 12 of 77PIN: ________

    Job Title: ____________________

    Section Properties

    Area of Section: AAA LAA1t gp AAA 101 in2

    Moment of Inertia of Section: IAA1

    12

    tgp LAA13

    IAA 68800 in4

    Neutral Axis: xNA .5LAA1 xNA 45.1 in

    Section Modulus of Section:SAA.left

    IAA

    xNA SAA.left 1526 in

    3

    SAA.right

    IAA

    xNA

    SAA.right 1526in3

    Moment Arms: eAA.B XA1 xNA YA1tanB eAA.B 16.677 in

    eAA.C XA1 xNA YA1tanC eAA.C 1.3in

    eAA.D XA1 xNA YA1tan D eAA.D 17.9 in

    Forces Acting on Section

    Case 1

    Axial Force: FAA1 FB1y FC1y FD1y FAA1 170 kip

    Shear Force: VAA1 FB1x FC1x FD1x VAA1 218 kip

    Bending Moment: MAA1 FB1yeAA.B FC1yeAA.C FD1yeAA.D MAA1 4050 kip in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    J o i n t L 4

    Sheet: 13 of 77PIN: ________

    Job Title: ____________________

    Case 2

    Axial Force: FAA2 FB2y FC2y FD2y FAA2 210 kip

    Shear Force: VAA2 FB2x FC2x FD2x VAA2 223 kip

    Bending Moment: MAA2 FB2yeAA.B FC2yeAA.C FD2yeAA.D MAA2 4096 kip in

    Case 3

    Axial Force: FAA3 FB3y FC3y FD3y FAA3 178 kip

    Shear Force: VAA3 FB3x FC3x FD3x VAA3 233 kip

    Bending Moment: MAA3 FB3yeAA.B FC3yeAA.C FD3yeAA.D MAA3 4334 kip in

    Case 4

    Axial Force: FAA4 FB4y FC4y FD4y FAA4 195 kip

    Shear Force: VAA4 FB4x FC4x FD4x VAA4 222 kip

    Bending Moment: MAA4 FB4yeAA.B FC4yeAA.C FD4yeAA.D MAA4 4098 kip in

    Stress Along Section

    Case 1

    Axial Stress: AA1.a

    FAA1

    AAA

    AA1.a 1.7ksi

    Flexural Stress: AA1.b.left

    MAA1

    SAA.left

    AA1.b.left 2.7ksi

    AA1.b.right

    MAA1

    SAA.right

    AA1.b.right 2.7 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 14 of 77PIN: ________

    Job Title: ____________________

    Uniform Average Shear Stress: AA1.vu

    VAA1

    AAA

    AA1.vu 2.1 ksi

    Maximum Average Shear Stress: AA1.v QLAA1

    2tgp

    LAA1

    4

    VAA1Q

    IAAtgp

    AA1.v 3.2 ksi

    Case 2

    Axial Stress: AA2.a

    FAA2

    AAA

    AA2.a 2.1ksi

    Flexural Stress: AA2.b.left

    MAA2

    SAA.left

    AA2.b.left 2.7ksi

    AA2.b.right

    MAA2

    SAA.right

    AA2.b.right 2.7 ksi

    Uniform Average Shear Stress: AA2.vu

    VAA2

    AAA

    AA2.vu 2.2 ksi

    Maximum Average Shear Stress: AA2.v QLAA1

    2tgp

    LAA1

    4

    VAA2Q

    IAAtgp

    AA2.v 3.3 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 15 of 77PIN: ________

    Job Title: ____________________

    Case 3

    Axial Stress: AA3.a

    FAA3

    AAA AA3.a 1.8ksi

    Flexural Stress: AA3.b.left

    MAA3

    SAA.left

    AA3.b.left 2.8ksi

    AA3.b.right

    MAA3

    SAA.right

    AA3.b.right 2.8 ksi

    Uniform Average Shear Stress: AA3.vuVAA3

    AAA

    AA3.vu 2.3 ksi

    Maximum Average Shear Stress: AA3.v QLAA1

    2tgp

    LAA1

    4

    VAA3Q

    IAAtgp

    AA3.v 3.4 ksi

    Case 4

    Axial Stress: AA4.a

    FAA4

    AAA

    AA4.a 1.9ksi

    Flexural Stress: AA4.b.left

    MAA4

    SAA.left

    AA4.b.left 2.7ksi

    AA4.b.right

    MAA4

    SAA.right

    AA4.b.right 2.7 ksi

    Uniform Average Shear Stress: AA4.vu

    VAA4

    AAA

    AA4.vu 2.2 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 16 of 77PIN: ________

    Job Title: ____________________

    Maximum Average Shear Stress: AA4.v QLAA1

    2tgp

    LAA1

    4

    VAA4Q

    IAAtgp

    AA4.v 3.3 ksi

    Comparing Section A1-A1 Stresses to LRFD Allowable

    Radius of Gyration of Gusset Plate: rgp

    tgp

    12

    rgp 0.325in

    Compressive Stress on Side Edges

    C1 L1 AA1.a AA1.b.left

    L2 AA2.a AA2.b.left

    L3 AA3.a AA3.b.left

    L4 AA4.a AA4.b.left

    c min L1 L2 L3 L4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    C4 R1 AA1.a AA1.b.right

    R2 AA2.a AA2.b.right

    R3 AA3.a AA3.b.right

    R4 AA4.a AA4.b.right

    c min R1 R2 R3 R4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    C1 0.0ksi C4 1.1 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 17 of 77PIN: ________

    Job Title: ____________________

    Allowable Compressive Stress LRFD 6.9.4.1

    C.all.1 Lc B1

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.1 23.2 ksi

    C.all.4 Lc B4

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.4 22.8 ksi

    Capacity/Demand

    CD1 99return C1 0ksi=if

    C.all.1

    C1return otherwise

    CD1 99.00 al1 C.all.1

    ac1 C1

    CD2 99return C4 0ksi=if

    C.all.4

    C4return otherwise

    CD2 20.93 al2 C.all.4

    ac2 C4

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 18 of 77PIN: ________

    Job Title: ____________________

    Tensile Stress on Side Edges

    T1 L1 AA1.a AA1.b.left

    L2 AA2.a AA2.b.left

    L3 AA3.a AA3.b.left

    L4 AA4.a AA4.b.left

    c max L1 L2 L3 L4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T4 R1 AA1.a AA1.b.right

    R2 AA2.a AA2.b.right

    R3 AA3.a AA3.b.right

    R4 AA4.a AA4.b.right

    c max R1 R2 R3 R4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T1 4.8ksi T4 0.0ksi

    Allowable Tensile Stress LRFD 6.14.2.8

    T.all fFy T.all 50ksi

    Capacity/Demand

    al3 T.allCD3 99return T1 0ksi=if

    T.all

    T1return otherwise

    CD3 10.52ac3 T1

    CD4 99return T4 0ksi=if

    T.all

    T4return otherwise

    CD4 99.00 al4 T.all

    ac4 T4

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 19 of 77PIN: ________

    Job Title: ____________________

    Allowable Shear Stress on Section A1-A1 LRFD 6.14.2.8

    xy.all

    v.74 Fy

    3 xy.all 21.4 ksi

    Calculated Maximum Average Shear Stress

    xy.max max AA1.v AA2.v AA3.v AA4.v xy.max 3.4ksi

    Capacity/Demand

    al5 xy.allCD5

    xy.all

    xy.max CD5 6.21

    ac5 xy.max

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 20 of 77PIN: ________

    Job Title: ____________________

    Analysis of Horizontal Section A2-A2

    LAA2 90.2in

    YA2 7.0in

    XA2 46.4in

    Number of Bolt Holes Along Section Cut in Gusset Plate: NAgp 24

    Force Diagram

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 21 of 77PIN: ________

    Job Title: ____________________

    Section Properties

    Gross Area of Section: AAA LAA2t gp AAA 101 in2

    Net Area of Section: AAAn LAA2 NAgpd h tgp hsptsp AAAn 86in2

    Ratio of Gross to Net Area: Rgn

    AAA

    AAAn

    Rgn 1.183

    Moment of Inertia of Section: IAA1

    12

    tgp LAA23

    IAA 68800 in4

    Neutral Axis: xNA .5LAA2 xNA 45.1 in

    Section Modulus of Section:SAA.left

    IAA

    xNA SAA.left 1526 in

    3

    SAA.right

    IAA

    xNA

    SAA.right 1526in3

    Moment Arms: eAA.B XA2 xNA YA2tanB eAA.B 5.114 in

    eAA.C XA2 xNA YA2tanC eAA.C 1.3in

    eAA.D XA2 xNA YA2tan D eAA.D 7.2in

    Forces Acting on Section

    Case 1

    Axial Force: FAA1 FB1y FC1y FD1y FAA1 170 kip

    Shear Force: VAA1 FB1x FC1x FD1x VAA1 218 kip

    Bending Moment: MAA1 FB1yeAA.B FC1yeAA.C FD1yeAA.D MAA1 1303 kip in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 22 of 77PIN: ________

    Job Title: ____________________

    Case 2

    Axial Force: FAA2 FB2y FC2y FD2y FAA2 210 kip

    Shear Force: VAA2 FB2x FC2x FD2x VAA2 223 kip

    Bending Moment: MAA2 FB2yeAA.B FC2yeAA.C FD2yeAA.D MAA2 1286 kip in

    Case 3

    Axial Force: FAA3 FB3y FC3y FD3y FAA3 178 kip

    Shear Force: VAA3 FB3x FC3x FD3x VAA3 233 kip

    Bending Moment: MAA3 FB3yeAA.B FC3yeAA.C FD3yeAA.D MAA3 1398 kip in

    Case 4

    Axial Force: FAA4 FB4y FC4y FD4y FAA4 195 kip

    Shear Force: VAA4 FB4x FC4x FD4x VAA4 222 kip

    Bending Moment: MAA4 FB4yeAA.B FC4yeAA.C FD4yeAA.D MAA4 1299 kip in

    Stress Along Section

    Case 1

    Axial Stress: AA1.a

    FAA1

    AAA

    AA1.a 1.7ksi

    Flexural Stress: AA1.b.left

    MAA1

    SAA.left

    AA1.b.left 0.9ksi

    AA1.b.right

    MAA1

    SAA.right

    AA1.b.right 0.9 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 23 of 77PIN: ________

    Job Title: ____________________

    Uniform Average Shear Stress: AA1.vu

    VAA1

    AAA

    AA1.vu 2.1 ksi

    Maximum Average Shear Stress: AA1.v QLAA2

    2tgp

    LAA2

    4

    VAA1Q

    IAAtgp

    AA1.v 3.2 ksi

    Case 2

    Axial Stress: AA2.aFAA2

    AAA

    AA2.a 2.1ksi

    Flexural Stress: AA2.b.left

    MAA2

    SAA.left

    AA2.b.left 0.8ksi

    AA2.b.right

    MAA2

    SAA.right

    AA2.b.right 0.8 ksi

    Uniform Average Shear Stress: AA2.vu

    VAA2

    AAA

    AA2.vu 2.2 ksi

    Maximum Average Shear Stress: AA2.v QLAA2

    2tgp

    LAA2

    4

    VAA2Q

    IAAtgp

    AA2.v 3.3 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 24 of 77PIN: ________

    Job Title: ____________________

    Case 3

    Axial Stress: AA3.a

    FAA3

    AAA AA3.a 1.8ksi

    Flexural Stress: AA3.b.left

    MAA3

    SAA.left

    AA3.b.left 0.9ksi

    AA3.b.right

    MAA3

    SAA.right

    AA3.b.right 0.9 ksi

    Uniform Average Shear Stress: AA3.vuVAA3

    AAA

    AA3.vu 2.3 ksi

    Maximum Average Shear Stress: AA3.v QLAA2

    2tgp

    LAA2

    4

    VAA3Q

    IAAtgp

    AA3.v 3.4 ksi

    Case 4

    Axial Stress: AA4.a

    FAA4

    AAA

    AA4.a 1.9ksi

    Flexural Stress: AA4.b.left

    MAA4

    SAA.left

    AA4.b.left 0.9ksi

    AA4.b.right

    MAA4

    SAA.right

    AA4.b.right 0.9 ksi

    Uniform Average Shear Stress: AA4.vu

    VAA4

    AAA

    AA4.vu 2.2 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    29/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 25 of 77PIN: ________

    Job Title: ____________________

    Maximum Average Shear Stress: AA4.v QLAA2

    2tgp

    LAA2

    4

    VAA4Q

    IAAtgp

    AA4.v 3.3 ksi

    Comparing Section A2-A2 Stresses to LRFD Allowable

    Radius of Gyration of Gusset Plate: rgp

    tgp

    12

    rgp 0.325in

    Compressive Stress on Side Edges

    2C1 L1 AA1.a AA1.b.left

    L2 AA2.a AA2.b.left

    L3 AA3.a AA3.b.left

    L4 AA4.a AA4.b.left

    c min L1 L2 L3 L4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    2C4 R1 AA1.a AA1.b.right

    R2 AA2.a AA2.b.right

    R3 AA3.a AA3.b.right

    R4 AA4.a AA4.b.right

    c min R1 R2 R3 R4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    2C1 0.0ksi 2C4 0.0ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 26 of 77PIN: ________

    Job Title: ____________________

    Allowable Compressive Stress LRFD 6.9.4.1

    C.all.1 Lc B1

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.1 23.2 ksi

    C.all.4 Lc B4

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.4 22.8 ksi

    Capacity/Demand

    CD6 99return 2C1 0ksi=if

    C.all.1

    2C1return otherwise

    CD6 99.00 al6 C.all.1

    ac6 2C1

    CD7 99return 2C4 0ksi=if

    C.all.4

    2C4

    return otherwise

    CD7 99.00 al7 C.all.4

    ac7 2C4

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 27 of 77PIN: ________

    Job Title: ____________________

    Tensile Stress on Side Edges

    T1.g L1 AA1.a AA1.b.left

    L2 AA2.a AA2.b.left

    L3 AA3.a AA3.b.left

    L4 AA4.a AA4.b.left

    c max L1 L2 L3 L4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T4.g R1 AA1.a AA1.b.right

    R2 AA2.a AA2.b.right

    R3 AA3.a AA3.b.right

    R4 AA4.a AA4.b.right

    c max R1 R2 R3 R4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T1.g 2.9ksi T4.g 1.2ksi

    T1.n L1 AA1.aRgn AA1.b.left

    L2 AA2.aRgn AA2.b.left

    L3 AA3.aRgn AA3.b.left

    L4 AA4.aRgn AA4.b.left

    c max L1 L2 L3 L4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T4.n R1 AA1.aRgn AA1.b.right

    R2 AA2.aRgn AA2.b.right

    R3 AA3.aRgn AA3.b.right

    R4 AA4.aRgn AA4.b.right

    c max R1 R2 R3 R4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T1.n 3.3ksi T4.n 1.6ksi

    Allowable Tensile Stress on Gross Section LRFD 6.8.2

    T.all.g yFy T.all.g 47ksi

    Allowable Tensile Stress on Net Section LRFD 6.8.2

    T.all.n uFu U T.all.n 52ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 28 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    T1.g 0ksi=if

    all1 T.all.g

    act1 T1.g

    fs1all1

    act1

    all2 T.all.n

    act2 T1.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m2

    all1

    ksi fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD8 f11 f2

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    T4.g 0ksi=if

    all1 T.all.g

    act1 T4.g

    fs1all1

    act1

    all2 T.all.n

    act2 T4.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m2

    all1

    ksi fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD9 f21

    al8 f12 al9 f22

    ac8 f13 ac9 f23

    CD8 15.81 CD9 32.45

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    33/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 29 of 77PIN: ________

    Job Title: ____________________

    Allowable Shear Stress on Gross Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.g vy.58 Fy .74 xy.all.g 20.4ksi

    Allowable Shear Stress on Net Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.n vu.58 Fu .74 xy.all.n 22.3 ksi

    Calculated Maximum Average Shear Stress

    xy.max.g max AA1.v AA2.v AA3.v AA4.v xy.max.g 3.4ksi

    xy.max.n xy.max.g Rgn xy.max.n 4.1ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    34/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 30 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    xy.max.g 0ksi=if

    all1 xy.all.g

    act1 xy.max.g

    fs1all1

    act1

    all2 xy.all.n

    act2 xy.max.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m

    2

    all1

    ksi

    fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD10 f11

    al10 f12

    ac10 f13

    CD10 5.48

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    35/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 31 of 77PIN: ________

    Job Title: ____________________

    Analysis of Vertical Section B-B

    LBB 59.4in

    XB 6.339in

    YB 9.842in

    NBI 50

    NBE 10

    Number of Bolt Holes Along Section Cut in Gusset Plate: NBgp 11

    Number of Bolt Holes Along Section Cut in Splice Plate: NBsp 5

    Force Diagram

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 32 of 77PIN: ________

    Job Title: ____________________

    NBT NBI NBE NBT 60

    Section Properties

    Gross Area of Section: ABB LBBtgp hspt sp ABB 80in2

    Net Area of Section: ABBn LBB NBgpdh tgp hsp NBspd h tsp ABBn 63in2

    Ratio of Gross to Net Area: Rgn

    ABB

    ABBn

    Rgn 1.273

    Bottom of Gusset Plate to Neutral Axis: yNA Agp tgpLBB

    Asp tsphsp

    y

    AgpLBB

    2

    Asp Lgs

    hsp

    2

    Agp Asp

    yreturn

    yNA 27in

    Moment of Inertia of Section: IBB Igp 1

    12tgp LBB

    3

    Isp 1

    12tsp hsp

    3

    ygpLBB

    2

    ysp Lgs

    hsp

    2

    I Igp tgpLBB yNA ygp 2

    Isp tsph sp yNA ysp 2

    Ireturn

    IBB 24083 in4

    Section Modulus of Section:SBB.top

    IBB

    yNA LBB SBB.top 733 in

    3

    SBB.bot

    IBB

    yNA

    SBB.bot 907in3

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    37/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 33 of 77PIN: ________

    Job Title: ____________________

    Moment Arms: eBB.D yNA

    XB

    tan D

    YB

    eBB.D 9.2in

    eBB.E yNA

    XB

    tan E YB

    eBB.E 16.7 in

    Forces Acting on Section

    Case 1

    Axial Force: FBB1 FD1x FE1x

    NBT

    NBE

    NBT

    FBB1 1508kip

    Shear Force: VBB1 FD1y FE1y

    NBT NBE

    NBT

    VBB1 28 kip

    Bending Moment: MBB1 FD1xeBB.D FE1x

    NBT NBE

    NBT

    eBB.E MBB1 25351 kip in

    Case 2

    Axial Force: FBB2 FD2x FE2x

    NBT NBE

    N

    BT

    FBB2 1456kip

    Shear Force: VBB2 FD2y FE2y

    NBT NBE

    NBT

    VBB2 10 kip

    Bending Moment: MBB2 FD2xeBB.D FE2x

    NBT NBE

    NBT

    eBB.E MBB2 24375 kip in

    Case 3

    Axial Force: FBB3 FD3x FE3x

    NBT NBE

    NBT

    FBB3 1429kip

    Shear Force: VBB3 FD3y FE3y

    NBT

    NBE

    NBT

    VBB3 32 kip

    Bending Moment: MBB3 FD3xeBB.D FE3x

    NBT NBE

    NBT

    eBB.E MBB3 24070 kip in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 34 of 77PIN: ________

    Job Title: ____________________

    Case 4

    Axial Force: FBB4 FD4x FE4x

    NBT NBE

    NBT

    FBB4 1440kip

    Shear Force: VBB4 FD4y FE4y

    NBT NBE

    NBT

    VBB4 17 kip

    Bending Moment: MBB4 FD4xeBB.D FE4x

    NBT NBE

    NBT

    eBB.E MBB4 24158 kip in

    Stress Along Section

    Case 1

    Axial Stress: BB1.a

    FBB1

    ABB

    BB1.a 18.9 ksi

    Flexural Stress: BB1.b.top

    MBB1

    SBB.top

    BB1.b.top 34.6 ksi

    BB1.b.bot

    MBB1

    SBB.bot

    BB1.b.bot 27.9ksi

    Uniform Average Shear Stress: BB1.vu

    VBB1

    ABB

    BB1.vu 0.3 ksi

    Maximum Average Shear Stress: BB1.v Q1 yNAtgp yNA

    2

    Q2 h

    sp

    t

    sp

    y

    NA

    L

    gs

    hsp

    2

    Q Q1 Q2

    VBB1Q

    IBBtgp

    return

    BB1.v 0.6 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 35 of 77PIN: ________

    Job Title: ____________________

    Case 2

    Axial Stress: BB2.aFBB2

    ABB

    BB2.a 18.2 ksi

    Flexural Stress: BB2.b.top

    MBB2

    SBB.top

    BB2.b.top 33.3 ksi

    BB2.b.bot

    MBB2

    SBB.bot

    BB2.b.bot 26.9ksi

    Uniform Average Shear Stress: BB2.vuVBB2

    ABB

    BB2.vu 0.1 ksi

    Maximum Average Shear Stress: BB2.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB2QIBBtgp

    return

    BB2.v 0.2 ksi

    Case 3

    Axial Stress: BB3.a

    FBB3

    ABB

    BB3.a 17.9 ksi

    Flexural Stress: BB3.b.top

    MBB3

    SBB.top BB3.b.top 32.8 ksi

    BB3.b.bot

    MBB3

    SBB.bot

    BB3.b.bot 26.5ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 36 of 77PIN: ________

    Job Title: ____________________

    Uniform Average Shear Stress: BB3.vu

    VBB3

    ABB

    BB3.vu 0.4 ksi

    Maximum Average Shear Stress: BB3.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB3Q

    IBBtgp

    return

    BB3.v 0.7 ksi

    Case 4

    Axial Stress: BB4.a

    FBB4

    ABB

    BB4.a 18.1 ksi

    Flexural Stress: BB4.b.top

    MBB4

    SBB.top

    BB4.b.top 33.0 ksi

    BB4.b.bot

    MBB4

    SBB.bot

    BB4.b.bot 26.6ksi

    Uniform Average Shear Stress: BB4.vu

    VBB4

    ABB

    BB4.vu 0.2 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 37 of 77PIN: ________

    Job Title: ____________________

    Maximum Average Shear Stress: BB4.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB4Q

    IBBtgp

    return

    BB4.v 0.4 ksi

    Comparing Section B-B Stresses to LRFD Allowable

    Compressive Stress on Top Edge

    C3 T1 BB1.a BB1.b.top

    T2 BB2.a BB2.b.top

    T3 BB3.a BB3.b.top

    T4 BB4.a BB4.b.top

    c min T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    C3 15.7 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 38 of 77PIN: ________

    Job Title: ____________________

    Allowable Compressive Stress LRFD 6.9.4.1

    C.all.3 Lc B3

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.3 29.3 ksi

    Capacity/Demand

    al11 C.all.3CD11 99return C3 0ksi=if

    C.all.3

    C3return otherwise

    CD11 1.86 ac11 C3

    Tensile Stress on Edges

    Tbr.g B1 BB1.a BB1.b.bot

    B2 BB2.a BB2.b.bot

    B3 BB3.a BB3.b.bot

    B4 BB4.a BB4.b.bot

    c max B1 B2 B3 B4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T3.g T1 BB1.a BB1.b.top

    T2 BB2.a BB2.b.top

    T3 BB3.a BB3.b.top

    T4 BB4.a BB4.b.top

    c max T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    Tbr.g 46.8ksi T3.g 0.0ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 39 of 77PIN: ________

    Job Title: ____________________

    Tbr.n B1 BB1.aRgn BB1.b.bot

    B2 BB2.aRgn BB2.b.botB3 BB3.aRgn BB3.b.bot

    B4 BB4.aRgn BB4.b.bot

    c max B1 B2 B3 B4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T3.n T1 BB1.aRgn BB1.b.top

    T2 BB2.aRgn BB2.b.topT3 BB3.aRgn BB3.b.top

    T4 BB4.aRgn BB4.b.top

    c max T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    Tbr.n 52.0 ksi T3.n 0.0ksi

    Allowable Tensile Stress on Gross Section LRFD 6.8.2

    T.all.g yFy T.all.g 47ksi

    Allowable Tensile Stress on Net Section LRFD 6.8.2

    T.all.n uFu U T.all.n 52ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 40 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    Tbr.g 0ksi=if

    all1 T.all.g

    act1 Tbr.g

    fs1all1

    act1

    all2 T.all.n

    act2 Tbr.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m2

    all1

    ksi fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD12 f11 f2

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    T3.g 0ksi=if

    all1 T.all.g

    act1 T3.g

    fs1all1

    act1

    all2 T.all.n

    act2 T3.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m2

    all1

    ksi fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD13 f21

    al12 f12 al13 f22

    ac12 f13 ac13 f23

    CD12 1.00 CD13 99.00

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 41 of 77PIN: ________

    Job Title: ____________________

    Allowable Shear Stress on Gross Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.g vy.58 Fy .74 xy.all.g 20.4ksi

    Allowable Shear Stress on Net Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.n vu.58 Fu .74 xy.all.n 22.3 ksi

    Calculated Maximum Average Shear Stress

    xy.max.g max BB1.v BB2.v BB3.v BB4.v xy.max.g 0.7ksi

    xy.max.n xy.max.g Rgn xy.max.n 0.9ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 42 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    xy.max.g 0ksi=if

    all1 xy.all.g

    act1 xy.max.g

    fs1all1

    act1

    all2 xy.all.n

    act2 xy.max.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m

    2

    all1

    ksi

    fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD14 f11

    al14 f12

    ac14 f13

    CD14 24.22

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    State of New York

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 43 of 77PIN: ________

    Job Title: ____________________

    Analysis of Vertical Section C-C

    LCC 59.4in

    XC 6.339in

    YC 9.842in

    NCI 50

    NCE 10

    Number of Bolt Holes Along Section Cut in Gusset Plate: NCgp 11

    Number of Bolt Holes Along Section Cut in Splice Plate: NCsp 5

    Force Diagram

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 44 of 77PIN: ________

    Job Title: ____________________

    LBB LCC NCT NCI NCE

    FD1x FB1x FE1x FA1x FD2x FB2x FE2x FA2x

    FD1y FB1y FE1y FA1y FD2y FB2y FE2y FA2y

    FD3x FB3x FE3x FA3x FD4x FB4x FE4x FA4x

    FD3y FB3y FE3y FA3y FD4y FB4y FE4y FA4y

    Section Properties

    Gross Area of Section: ABB LBBtgp hspt sp ABB 80in2

    Net Area of Section: ABBn LBB NBgpdh tgp hsp NBspd h tsp ABBn 63in2

    Ratio of Gross to Net Area: Rgn

    ABB

    ABBn

    Rgn 1.273

    Bottom of Gusset Plate to Neutral Axis: yNA Agp tgpLBB

    Asp t

    sp

    h

    sp

    y

    AgpLBB

    2

    Asp Lgs

    hsp

    2

    Agp Asp

    yreturn

    yNA 27in

    Moment of Inertia of Section: IBB Igp 1

    12tgp LBB

    3

    Isp 1

    12tsp hsp

    3

    ygpLBB

    2

    ysp Lgs

    hsp

    2

    I Igp tgpLBB yNA ygp 2

    Isp tsph sp yNA ysp 2

    Ireturn

    IBB 24083 in4

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 45 of 77PIN: ________

    Job Title: ____________________

    Section Modulus of Section:SBB.top

    IBB

    yNA LBB SBB.top 733 in

    3

    SBB.bot

    IBB

    yNA

    SBB.bot 907in3

    Moment Arms: eCC.B yNA YC XC

    tan B eCC.B 9.8in

    eCC.A yNA YC XC

    tan A eCC.A 16.7 in

    eBB.D eCC.B eBB.E eCC.A

    Forces Acting on Section

    Case 1

    Axial Force: FBB1 FD1x FE1x

    NCT NCE

    NCT

    FBB1 1552kip

    Shear Force: VBB1 FD1y FE1y

    NCT NCE

    NCT

    VBB1 212 kip

    Bending Moment: MBB1 FD1xeBB.D FE1x

    NCT NCE

    NCT

    eBB.E MBB1 24575 kip in

    Case 2

    Axial Force: FBB2 FD2x FE2x

    NCT NCE

    NCT

    FBB2 1519kip

    Shear Force: VBB2

    F

    D2y

    F

    E2y

    NCT NCE

    NCT

    V

    BB2

    234 kip

    Bending Moment: MBB2 FD2xeBB.D FE2x

    NCT NCE

    NCT

    eBB.E MBB2 23874 kip in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 46 of 77PIN: ________

    Job Title: ____________________

    Case 3

    Axial Force: FBB3 FD3x FE3xNCT NCE

    NCT

    FBB3 1483kip

    Shear Force: VBB3 FD3y FE3y

    NCT NCE

    NCT

    VBB3 224 kip

    Bending Moment: MBB3 FD3xeBB.D FE3x

    NCT NCE

    NCT

    eBB.E MBB3 23334 kip in

    Case 4

    Axial Force: FBB4 FD4x FE4x

    NCT NCE

    NCT

    FBB4 1492kip

    Shear Force: VBB4 FD4y FE4y

    NCT NCE

    NCT

    VBB4 226 kip

    Bending Moment: MBB4 FD4xeBB.D FE4x

    NCT NCE

    NCT

    eBB.E MBB4 23481 kip in

    Stress Along Section

    Case 1

    Axial Stress: BB1.aFBB1

    ABB

    BB1.a 19.5 ksi

    Flexural Stress: BB1.b.top

    MBB1

    SBB.top

    BB1.b.top 33.5 ksi

    BB1.b.bot

    MBB1

    SBB.bot

    BB1.b.bot 27.1ksi

    Uniform Average Shear Stress: BB1.vu

    VBB1

    ABB

    BB1.vu 2.7 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 47 of 77PIN: ________

    Job Title: ____________________

    Maximum Average Shear Stress: BB1.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB1Q

    IBBtgp

    return

    BB1.v 4.8 ksi

    Case 2

    Axial Stress: BB2.a

    FBB2

    ABB

    BB2.a 19.0 ksi

    Flexural Stress: BB2.b.top

    MBB2

    SBB.top

    BB2.b.top 32.6 ksi

    BB2.b.bot

    MBB2

    SBB.bot

    BB2.b.bot 26.3ksi

    Uniform Average Shear Stress: BB2.vu

    VBB2

    ABB

    BB2.vu 2.9 ksi

    Maximum Average Shear Stress: BB2.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB2Q

    IBBtgp

    return

    BB2.v 5.2 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 48 of 77PIN: ________

    Job Title: ____________________

    Case 3

    Axial Stress: BB3.aFBB3

    ABB

    BB3.a 18.6 ksi

    Flexural Stress: BB3.b.top

    MBB3

    SBB.top

    BB3.b.top 31.8 ksi

    BB3.b.bot

    MBB3

    SBB.bot

    BB3.b.bot 25.7ksi

    Uniform Average Shear Stress: BB3.vu

    VBB3

    ABB

    BB3.vu 2.8 ksi

    Maximum Average Shear Stress: BB3.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB3Q

    IBBtgp

    return

    BB3.v 5.0 ksi

    Case 4

    Axial Stress: BB4.a

    FBB4

    ABB

    BB4.a 18.7 ksi

    Flexural Stress: BB4.b.top

    MBB4

    SBB.top

    BB4.b.top 32.0 ksi

    BB4.b.bot

    MBB4

    SBB.bot

    BB4.b.bot 25.9ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 49 of 77PIN: ________

    Job Title: ____________________

    Uniform Average Shear Stress: BB4.vu

    VBB4

    ABB

    BB4.vu 2.8 ksi

    Maximum Average Shear Stress: BB4.v Q1 yNAtgp yNA

    2

    Q2 hspt sp yNA Lgshsp

    2

    Q Q1 Q2

    VBB4Q

    I

    BB

    t

    gp

    return

    BB4.v 5.1 ksi

    Comparing Section C-C Stresses to LRFD Allowable

    Compressive Stress on Top Edge

    C2 T1 BB1.a BB1.b.top

    T2 BB2.a BB2.b.top

    T3 BB3.a BB3.b.top

    T4 BB4.a BB4.b.top

    c min T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    C2 14.1 ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 50 of 77PIN: ________

    Job Title: ____________________

    Allowable Compressive Stress LRFD 6.9.4.1

    C.all.2 Lc B2

    K Lc

    rgp

    2 Fy

    E

    c 0.66

    Fy 2.25if

    c0.88 Fy

    otherwise

    C.all.2 26.2 ksi

    Capacity/Demand

    al15 C.all.2CD15 99return C2 0ksi=if

    C.all.2

    C2return otherwise

    CD15 1.86 ac15 C2

    Tensile Stress on Edges

    Tbl.g B1 BB1.a BB1.b.bot

    B2 BB2.a BB2.b.bot

    B3 BB3.a BB3.b.bot

    B4 BB4.a BB4.b.bot

    c max B1 B2 B3 B4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T2.g T1 BB1.a BB1.b.top

    T2 BB2.a BB2.b.top

    T3 BB3.a BB3.b.top

    T4 BB4.a BB4.b.top

    c max T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    Tbl.g 46.5ksi T2.g 0.0ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 51 of 77PIN: ________

    Job Title: ____________________

    Tbl.n B1 BB1.aRgn BB1.b.bot

    B2 BB2.aRgn BB2.b.botB3 BB3.aRgn BB3.b.bot

    B4 BB4.aRgn BB4.b.bot

    c max B1 B2 B3 B4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    T2.n T1 BB1.aRgn BB1.b.top

    T2 BB2.aRgn BB2.b.topT3 BB3.aRgn BB3.b.top

    T4 BB4.aRgn BB4.b.top

    c max T1 T2 T3 T4( )

    n 0ksi

    nreturn c 0if

    creturn otherwise

    Tbl.n 51.9ksi T2.n 0.0ksi

    Allowable Tensile Stress on Gross Section LRFD 6.8.2

    T.all.g yFy T.all.g 47ksi

    Allowable Tensile Stress on Net Section LRFD 6.8.2

    T.all.n uFu U T.all.n 52ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 52 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    Tbl.g 0ksi=if

    all1 T.all.g

    act1 Tbl.g

    fs1all1

    act1

    all2 T.all.n

    act2 Tbl.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m

    2

    all1

    ksi

    fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD16 f11 f2

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    T2.g 0ksi=if

    all1 T.all.g

    act1 T2.g

    fs1all1

    act1

    all2 T.all.n

    act2 T2.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m

    2

    all1

    ksi

    fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD17 f21

    al16 f12 al17 f22

    ac16 f13 ac17 f23

    CD16 1.00 CD17 99.00

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 53 of 77PIN: ________

    Job Title: ____________________

    Allowable Shear Stress on Gross Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.g vy.58 Fy .74 xy.all.g 20.4ksi

    Allowable Shear Stress on Net Section FHWA Bridge Design Guidance No. 1, 2/28/08 Rev.

    xy.all.n vu.58 Fu .74 xy.all.n 22.3 ksi

    Calculated Maximum Average Shear Stress

    xy.max.g max BB1.v BB2.v BB3.v BB4.v xy.max.g 5.2ksi

    xy.max.n xy.max.g Rgn xy.max.n 6.7ksi

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 54 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    f1

    m1

    99

    m2

    "N/A"

    m3

    0

    mreturn

    xy.max.g 0ksi=if

    all1 xy.all.g

    act1 xy.max.g

    fs1all1

    act1

    all2 xy.all.n

    act2 xy.max.n

    fs2 all2

    act2

    m1

    min fs1 fs2( )

    m2

    all1

    ksi fs1 fs2if

    m2

    all2

    ksi otherwise

    m3

    act1

    ksi fs1 fs2if

    m3

    act2

    ksi otherwise

    mreturn

    CD18 f11

    al18 f12

    ac18 f13

    CD18 3.35

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 55 of 77PIN: ________

    Job Title: ____________________

    Unsupported Edge Requirement

    Allowable Length of Unsupported Edges

    ball 2.06 E

    Fy

    tgp ball 55.8 in LRFD 6.14.2.8

    Capacity/Demand

    al19 ballCD19

    ball

    B1 CD19 1.80

    ac19 B1

    al20 ballCD20

    ball

    B2

    CD20 1.99ac20 B2

    al21 ballCD21

    ball

    B3

    CD21 2.23ac21 B3

    al22 ballCD22

    ball

    B4

    CD22 1.78ac22 B4

    Edge Slenderness Ratio Requirement

    Allowable Slenderness Ratio: SRall 120 LRFD 6.9.3

    Calculated Slenderness Ratio

    SR1K B1

    rgp

    SR1 95

    SR2

    K B2

    rgp

    SR2 86

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 56 of 77PIN: ________

    Job Title: ____________________

    SR3

    K B3

    rgp

    SR3 77

    SR4

    K B4

    rgp

    SR4 97

    Capacity/Demand

    al23 if min C1 2C1 0 "N/A" SRall CD23 99return min C1 2C1 0if

    SRall

    SR1

    return otherwise

    CD23 99.00ac

    23

    if minC1

    2C1

    0 "N/A" SR

    1

    al24 if C2 0 "N/A" SRall CD24 99return C2 0ifSRall

    SR2

    return otherwise

    CD24 1.39ac24 if C2 0 "N/A" SR2

    al25 if C3 0 "N/A" SRall CD25 99return C3 0ifSRall

    SR3

    return otherwise

    CD25 1.56ac25 if C3 0 "N/A" SR3

    al26 if min C4 2C4 0 "N/A" SRall CD26 99return min C4 2C4 0ifSRall

    SR4

    return otherwise

    CD26 1.24ac26 if min C4 2C4 0 "N/A" SR4

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 57 of 77PIN: ________

    Job Title: ____________________

    Applied Force for Member Connection Analysis LRFD 6.13.1

    Maximum HL-93 Live

    Load + Impact Case 1

    Maximum HL-93 Live

    Load + Impact Case 2

    Member A AMHL1 499kip AMHL2 499kip

    Member B BMHL1 144kip BMHL2 80 kip

    Tensile +

    Compressive -Member C CMHL1 3kip CMHL2 3kip

    Member D DMHL1 118kip DMHL2 105 kip

    Member E EMHL1 546kip EMHL2 546kip

    Maximum Permit Live

    Load + Impact Case 3

    Maximum Permit Live

    Load + Impact Case 4

    Member A AMPV3 605kip AMPV4 605kip

    Member B BMPV3 196kip BMPV4 119 kip

    Tensile +

    Compressive -Member C CMPV3 4kip CMPV4 4kip

    Member D DMPV3 172kip DMPV4 150 kip

    Member E EMPV3 662kip EMPV4 662kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 58 of 77PIN: ________

    Job Title: ____________________

    Factored MemberResistance Case 1

    Factored MemberResistance Case 2

    Member A AR1 3894kip AR2 3894kip

    Member B BR1 1236kip BR2 1236kip

    Tensile +

    Compressive -Member C CR1 1435kip CR2 1435kip

    Member D DR1 2038kip DR2 927 kip

    Member E ER1 3894kip ER2 3894kip

    Maximum HL-93 Live Load + Impact Case 1: Enter the unfactored maximum member force due to HL-93 live load.

    If the member has both a tensile and compressive maximum, input the tensile maximum. Input tensile force as a

    positive value and compressive force as a negative value.

    Maximum HL-93 Live Load + Impact Case 2: Enter the unfactored maximum member force due to HL-93 live load.

    If the member has both a tensile and compressive maximum, input the compressive maximum. Input tensile force

    as a positive value and compressive force as a negative value.

    Maximum Permit Live Load + Impact Case 3: Enter the unfactored maximum member force due to permit live

    load. If the member has both a tensile and compressive maximum, input the tensile maximum. Input tensile force

    as a positive value and compressive force as a negative value.

    Maximum Permit Live Load + Impact Case 4: Enter the unfactored maximum member force due to permit live

    load. If the member has both a tensile and compressive maximum, input the compressive maximum. Input tensile

    force as a positive value and compressive force as a negative value.

    Factored Member Resistance Case 1: Enter the factored LRFD axial member resistance. If the member is

    subject to both tensile and compressive forces, input the tensile resistance. Input tensile resistance as a positive

    value and compressive resistance as a negative value.

    Factored Member Resistance Case 2: Enter the factored LRFD axial member resistance. If the member is

    subject to both tensile and compressive forces, input the compressive resistance. Input tensile resistance as a

    positive value and compressive resistance as a negative value.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 59 of 77PIN: ________

    Job Title: ____________________

    AM1 i 1.25ADC 1.5ADW 1.75 AMHL1 AM1 3414kipAM2 i 1.25ADC 1.5ADW 1.75 AMHL2 AM2 3414kipAM3 i 1.25ADC 1.5ADW 1.35 AMPV3 AM3 3355kipAM4 i 1.25ADC 1.5ADW 1.35 AMPV4 AM4 3355kip

    BM1 i 1.25BDC 1.5BDW 1.75 BMHL1 BM1 637 kipBM2 i 1.25BDC 1.5BDW 1.75 BMHL2 BM2 226 kipBM3 i 1.25BDC 1.5BDW 1.35 BMPV3 BM3 651 kipBM4 i 1.25BDC 1.5BDW 1.35 BMPV4 BM4 204 kip

    CM1 i 1.25CDC 1.5CDW 1.75 CMHL1 CM1 27 kipCM2 i 1.25CDC 1.5CDW 1.75 CMHL2 CM2 27 kipCM3 i 1.25CDC 1.5CDW 1.35 CMPV3 CM3 27 kipCM4 i 1.25CDC 1.5CDW 1.35 CMPV4 CM4 27 kip

    DM1 i 1.25DDC 1.5DDW 1.75 DMHL1 DM1 210 kipDM2 i 1.25DDC 1.5DDW 1.75 DMHL2 DM2 200 kipDM3 i 1.25DDC 1.5DDW 1.35 DMPV3 DM3 237 kipDM4 i 1.25DDC 1.5DDW 1.35 DMPV4 DM4 219 kip

    EM1 i 1.25EDC 1.5EDW 1.75 EMHL1 EM1 3721kipEM2 i 1.25EDC 1.5EDW 1.75 EMHL2 EM2 3721kipEM3 i 1.25EDC 1.5EDW 1.35 EMPV3 EM3 3656kipEM4 i 1.25EDC 1.5EDW 1.35 EMPV4 EM4 3656kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 60 of 77PIN: ________

    Job Title: ____________________

    PA1 f max AM1 AM3

    fa max mean f AR1 .75AR1 fareturn

    PA2 f min AM2 AM4

    fa min mean f AR2 .75AR2 fareturn

    PA1 3654kip PA2 2920kip

    PB1 f max BM1 BM3

    fa max mean f BR1 .75BR1

    fareturn

    PB2 f min BM2 BM4

    fa min mean f BR2 .75BR2

    fareturn

    PB1 943 kip PB2 720 kip

    PC1 f max CM1 CM3

    fa max mean f CR1 .75CR1

    fareturn

    PC2 f min CM2 CM4

    fa min mean f CR2 .75CR2

    fareturn

    PC1 1076kip PC2 704 kip

    PD1 f max DM1 DM3 fa max mean f DR1 .75DR1

    fareturn

    PD2 f min DM2 DM4 fa min mean f DR2 .75DR2

    fareturn

    PD1 1529kip PD2 695 kip

    PE2 f min EM2 EM4

    fa min mean f ER2 .75ER2

    fareturn

    PE1 f max EM1 EM3

    fa max mean f ER1 .75ER1

    fareturn

    PE2 2920kipPE1 3808kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 61 of 77PIN: ________

    Job Title: ____________________

    Slip Connection Applied Force LRFD 6.13.2.2

    PsA1 i 1.00ADC 1.00ADW 1.30 AMHL1 PsA1 2657kipPsA2 i 1.00ADC 1.00ADW 1.30 AMHL2 PsA2 2657kip

    PsB1 i 1.00BDC 1.00BDW 1.30 BMHL1 PsB1 492 kipPsB2 i 1.00BDC 1.00BDW 1.30 BMHL2 PsB2 186 kip

    PsC1 i 1.00CDC 1.00CDW 1.30 CMHL1 PsC1 22 kipPsC2 i 1.00CDC 1.00CDW 1.30 CMHL2 PsC2 22 kip

    PsD1 i 1.00DDC 1.00DDW 1.30 DMHL1 PsD1 156 kipPsD2 i 1.00DDC 1.00DDW 1.30 DMHL2 PsD2 149 kip

    PsE1 i 1.00EDC 1.00EDW 1.30 EMHL1 PsE1 2897kipPsE2 i 1.00EDC 1.00EDW 1.30 EMHL2 PsE2 2897kip

    Member Connection Resistance

    Number of Shear/Slip Planes Number of Bolts Bolt Clear Distance

    Member A Ns.A 2 NA 120 LcA 1.26in

    Member B Ns.B 1 NB 48 LcB 1.26in

    Member C Ns.C 1 NC 48 LcC 1.26in

    Member D Ns.D 1 ND 64 LcD 1.26in

    Member E Ns.E 2 NE 120 LcE 1.26in

    Number of Bolts: Input the total number of bolts connecting the member to the gusset plate. This

    includes bolts on both sides of the member.

    Bolt Clear Distance: Input the clear distance between the holes or between the hole and the edge of the

    material in the direction of the applied force.

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 62 of 77PIN: ________

    Job Title: ____________________

    Area of Bolt: Ab .25 db2

    Ab 0.785in2

    Resistance Factor for Bolts In Shear: sb 0.80 LRFD 6.5.4.2

    Bolt Group Shear Resistance LRFD 6.13.2.7

    Member A RA sb.38 Fub Ab NA Ns.A RA 6876kip

    Member B RB sb.38 Fub Ab NB Ns.B RB 1375kip

    Member C R

    C

    sb

    .38 Fub

    Ab

    NC

    Ns.C

    RC

    1375kip

    Member D RD sb.38 Fub Ab ND Ns.D RD 1834kip

    Member E RE sb.38 Fub Ab NE Ns.E RE 6876kip

    Note: If the length between extreme fasteners measured parallel to the line of action of the force is greater than

    50 inches, the above equations shall be multiplied by .80 per LRFD 6.13.2.7.

    Bolt Group Slip Resistance LRFD 6.13.2.8

    Hole size factor: Kh 1.0 LRFD 6.13.2.8-2

    Surface condition factor: Ks .33 LRFD 6.13.2.8-3

    Member A RsA KhKs Pt NA Ns.A RsA 4039kip

    Member B RsB KhKs Pt NB Ns.B RsB 808 kip

    Member C RsC KhKs Pt NC Ns.C RsC 808 kip

    Member D RsD KhKs Pt ND Ns.D RsD 1077kip

    Member E RsE KhKs Pt NE Ns.E RsE 4039kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 63 of 77PIN: ________

    Job Title: ____________________

    Bearing Resistance LRFD 6.13.2.9

    Resistance Factor for Bolts Bearing on Material: bb 0.80 LRFD 6.5.4.2

    Member A RbA bb1.2 LcA tgp tsp Fu NA RbA 17690kip

    Member B RbB bb1.2 LcB tgp Fu NB RbB 4246kip

    Member C RbC bb1.2 LcC tgp Fu NC RbC 4246kip

    Member D RbD bb1.2 LcD tgp Fu ND RbD 5661kip

    Member E RbE bb1.2 LcE tgp tsp Fu NE RbE 17690 kip

    Shear Capacity/Demand

    al27 RACD27

    RA

    max PA1 PA2 CD27 1.88

    ac27 max PA1 PA2

    al28 RBCD28

    RB

    max PB1 PB2 CD28 1.46

    ac28 max PB1 PB2

    al29 RCCD29

    RC

    max PC1 PC2 CD29 1.28

    ac29 max PC1 PC2

    al30 RDCD30

    RD

    max PD1 PD2 CD30 1.20

    ac30 max PD1 PD2

    al31 RECD31

    RE

    max PE1 PE2 CD31 1.81

    ac31 max PE1 PE2

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 64 of 77PIN: ________

    Job Title: ____________________

    Slip Capacity/Demand

    al32 RsACD32

    RsA

    max PsA1 PsA2 CD32 1.52

    ac32 max PsA1 PsA2

    al33 RsBCD33

    RsB

    max PsB1 PsB2 CD33 1.64

    ac33 max PsB1 PsB2

    al34 RsCCD34

    RsC

    max PsC1 PsC2 CD34 36.46

    ac34 max PsC1 PsC2

    al35 RsDCD35

    RsD

    max PsD1 PsD2 CD

    35

    6.91ac35 max PsD1 PsD2

    al36 RsECD36

    RsE

    max PsE1 PsE2 CD36 1.39

    ac36 max PsE1 PsE2

    Bearing Capacity/Demand

    al37 RbACD37

    RbA

    max PA1 PA2 CD37 4.84

    ac37 max PA1 PA2

    al38 RbBCD38

    RbB

    max PB1 PB2 CD38 4.50

    ac38 max PB1 PB2

    al39 RbCCD39

    RbC

    max PC1 PC2 CD39 3.94

    ac39 max PC1 PC2

    al40 RbDCD40

    RbD

    max PD1 PD2 CD40 3.70

    ac40 max PD1 PD2

    al41 RbECD41

    RbE

    max PE1 PE2 CD

    41

    4.65ac41 max PE1 PE2

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 65 of 77PIN: ________

    Job Title: ____________________

    Block Shear Rupture Resistance LRFD 6.13.4

    LvA 43.6in nbrA 5

    LvB 19.3in nbrB 4

    LvC 19.3in nbrC 4

    LvD 26.3in nbrD 4

    LvE 41.0in nbrE 5

    LtA 14.0in nrbA 11

    LtB 12.6in nrbB 6

    LtC 12.2in nrbC 6

    LtD 12.7in nrbD 8

    LtE 14.0in nrbE 11

    Gross Area Subject to Shear

    AvgA 2 LvA tgp 2 LvA tsp AvgA 163 in2

    AvgB 2 LvB tgp AvgB 43in2

    AvgC 2 LvC tgp AvgC 43in2

    AvgD 2 LvD tgp AvgD 59in2

    AvgE 2 LvE tgp 2 LvE tsp AvgE 154 in2

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 66 of 77PIN: ________

    Job Title: ____________________

    Net Area Subject to Shear

    AvnA 2 LvA nrbA .5 dh tgp 2 LvA nrbA .5 dh tsp AvnA 122 in2

    AvnB 2 LvB nrbB .5 dh tgp AvnB 30in2

    AvnC 2 LvC nrbC .5 dh tgp AvnC 30in2

    AvnD 2 LvD nrbD .5 dh tgp AvnD 41in2

    AvnE 2 LvE nrbE .5 dh tgp 2 LvE nrbE .5 dh tsp AvnE 112in2

    Gross Area Subject to Tension

    AtgA LtAt gp LtAt sp AtgA 26in2

    AtgB LtBtgp AtgB 14in2

    AtgC LtCtgp AtgC 14in2

    AtgD LtDt gp AtgD 14in

    2

    AtgE LtEtgp LtEtsp AtgE 26in2

    Net Area Subject to Tension

    AtnA LtA nbrA 1 dh tgp LtA nbrA 1 dh tsp AtnA 18in2

    AtnB LtB nbrB 1 dh tgp AtnB 11in2

    AtnC LtC nbrC 1 dh tgp AtnC 10in2

    AtnD LtD nbrD 1 dh tgp AtnD 11in2

    AtnE LtE nbrE 1 dh tgp LtE nbrE 1 dh tsp AtnE 18in2

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 67 of 77PIN: ________

    Job Title: ____________________

    Block Shear Rupture Resistance LRFD 6.13.4

    Strength Reduction Factor for Block Shear: bs 0.80 LRFD 6.5.4.2

    RrbsA bs 0.58 Fy AvgA FuAtnA AtnA 0.58 AvnAif

    bs 0.58 Fu AvnA FyAtgA otherwise

    RrbsA 4719kip

    RrbsB bs 0.58 Fy AvgB FuAtnB AtnB 0.58 AvnBif

    bs 0.58 Fu AvnB FyAtgB otherwise

    RrbsB 1480kip

    RrbsC bs 0.58 Fy AvgC FuAtnC AtnC 0.58 AvnCif

    bs 0.58 Fu AvnC FyAtgC otherwise

    RrbsC 1462kip

    RrbsD bs 0.58 Fy AvgD FuAtnD AtnD 0.58 AvnDifbs 0.58 Fu AvnD FyAtgD otherwise

    RrbsD 1815kip

    RrbsE bs 0.58 Fy AvgE FuAtnE AtnE 0.58 AvnEif

    bs 0.58 Fu AvnE FyAtgE otherwise

    RrbsE 4425kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 68 of 77PIN: ________

    Job Title: ____________________

    Capacity/Demand

    fA all R rbsA

    act .5PA1

    fs all

    act

    m1

    fs fs 0if

    m1

    99 otherwise

    m2

    all

    kip

    m3

    act

    kip fs 0if

    m3

    "N/A" otherwise

    mreturn

    CD42 fA1 fB all R rbsB

    act .5PB1

    fs all

    act

    m1

    fs fs 0if

    m1

    99 otherwise

    m2

    all

    kip

    m3

    act

    kip fs 0if

    m3

    "N/A" otherwise

    mreturn

    CD43 fB1

    al42 fA2 al43 fB2

    ac42 fA3 ac43 fB3

    CD42 2.58 CD43 3.14

    fC all R rbsC

    act .5PC1

    fs all

    act

    m1

    fs fs 0if

    m1

    99 otherwise

    m2

    all

    kip

    m3

    act

    kip fs 0if

    m3

    "N/A" otherwise

    mreturn

    CD44 fC1 fD all R rbsD

    act .5PD1

    fs all

    act

    m1

    fs fs 0if

    m1

    99 otherwise

    m2

    all

    kip

    m3

    act

    kip fs 0if

    m3

    "N/A" otherwise

    mreturn

    CD45 fD1

    al44 fC2 al45 fD2

    ac44 fC3 ac45 fD3

    CD44 2.72 CD45 2.38

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

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    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 69 of 77PIN: ________

    Job Title: ____________________

    fE all R rbsE

    act .5PE1

    fs all

    act

    m1

    fs fs 0if

    m1

    99 otherwise

    m2

    all

    kip

    m3

    act

    kip fs 0if

    m3

    "N/A" otherwise

    mreturn

    CD46 fE1

    al46 fE2

    ac46 fE3

    CD46 2.32

    Analysis of Whitmore Section

    LwA 39.2in

    LwB 32.9in

    LwC 32.4in

    LwD 41.0in

    LwE 39.2in

    LA 5.7in

    L

    B

    30.3in

    LC 23.2in

    LD 21.9in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

  • 8/10/2019 SDA-08-001 Gusset Plate Design

    74/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 70 of 77PIN: ________

    Job Title: ____________________

    Allowable Tensile Force on Gross Section LRFD 6.8.2

    PTGA yFy LwAtgp hspt sp PTGA 2711kip

    PTGB yFy LwBt gp PTGB 1758kip

    PTGC yFy LwCt gp PTGC 1731kip

    PTGD yFy LwDtgp PTGD 2191kip

    PTGE yFy LwEt gp hspt sp PTGE 2711kip

    Allowable Tensile Force on Net Section LRFD 6.8.2

    PTNA uFu U LwA nbrA 1 dh tgp LwA nbrA 1 dh tsp PTNA 3408kip

    PTNB uFu U LwB nbrB 1 dh tgp PTNB 1738kip

    PTNC uFu U LwC nbrC 1 dh tgp PTNC 1709kip

    PTND uFu U LwD nbrD 1 dh tgp PTND 2212kip

    PTNE uFu U LwE nbrE 1 dh tgp LwE nbrE 1 dh tsp PTNE 3408kip

    Controlling Allowable Tensile Force

    PTA min PTGA PTNA PTA 2711kip

    PTB min PTGB PTNB PTB 1738kip

    PTC min PTGC PTNC PTC 1709kip

    PTD min PTGD PTND PTD 2191kip

    PTE min PTGE PTNE PTE 2711kip

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

  • 8/10/2019 SDA-08-001 Gusset Plate Design

    75/81

    State of New York

    Department of Transportation

    L R F D G u s s e t P l a t e A n a l y s i s

    J o i n t L 4

    Sheet: 71 of 77PIN: ________

    Job Title: ____________________

    Gusset and Splice Plate Radius of Gyration

    w 1in

    yNA Agp tgpw

    Asp tspw

    y

    Agptgp

    2

    Asp tgp B

    tsp

    2

    Agp Asp

    yreturn

    yNA 2.0in

    IGS Igp 1

    12w tgp

    3

    Isp 1

    12w tsp

    3

    ygptgp

    2

    ysp tgp Btsp

    2

    I Igp tgpw yNA ygp 2

    Isp tspw yNA ysp 2

    Ireturn

    IGS 6 in4

    rgs

    IGS

    tgpw tspw rgs 1.757in

    Prep. By: J. Scarlata Date: 3/26/2008 Checked By: W. Albert Date: 4/2/2008

  • 8/10/2019 SDA-08-001 Gusset Plate D


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