plane trusses - university of michigan...continue moving across the truss, joint by joint. choose...

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Structures I University of Michigan, Taubman College Slide 1 of 31 Architecture 314 Structures I Plane Trusses Definition and Assumptions Nomenclature Stability and Determinacy Analysis by joints Analysis by sections Analysis and design by graphics 2 Force Members Pinned Joints Concurrent Member Centroids Joint Loaded Straight Members Small Deflections Bullring Covering, Xàtiva, Spain Kawaguchi and Engineers, 2007 Definitions and Assumtions Structures I University of Michigan, Taubman College Slide 2 of 31

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  • Structures I University of Michigan, Taubman College Slide 1 of 31

    Architecture 314

    Structures I

    Plane Trusses

    Definition and Assumptions

    Nomenclature

    Stability and Determinacy

    Analysis by joints

    Analysis by sections

    Analysis and design by graphics

    2 Force MembersPinned JointsConcurrent Member CentroidsJoint LoadedStraight MembersSmall Deflections

    Bullring Covering, Xàtiva, SpainKawaguchi and Engineers, 2007

    Definitions and Assumtions

    Structures I University of Michigan, Taubman College Slide 2 of 31

  • PanelsJoints

    • Upper: U1, U2, U3...• Lower: L1, L2, L3...

    Members• Chords• Web

    Nomenclature

    Structures I University of Michigan, Taubman College Slide 3 of 31

    2D Trusses• Concurrent Coplanar

    3D Trusses• Concurrent Non-Coplanar

    Force Systems

    University of Michigan Architectural Research LabUnistrut System, Charles W. Attwood

    Foster Bridge, 1889Ann Arbor, Michigan

    Structures I University of Michigan, Taubman College Slide 4 of 31

  • For:• j joints

    • m members

    • r reactions (restraints)

    Three conditions• m < k unstable

    • m = k stable and determinate

    • m > k stable and indeterminate

    Stability and Determinacy

    Structures I University of Michigan, Taubman College Slide 5 of 31

    Quiz

    For each of the following trusses, determine whether they are:

    A) StableB) Unstable

    • m < k unstable

    • m = k stable and determinate

    • m > k stable and indeterminate

    Truss 1

    Truss 2

    Structures I University of Michigan, Taubman College Slide 6/42

  • Not a true trussMoment frame structureRidgid joints as moment connectionsFlexure in members

    Vierendeel “Truss”

    Vierendeel bridge at Grammene, Belgium

    Photo by Karel Roose

    Salk Institute, La Jolla. Architect: Louis KahnEngineer: Komendant and Dubin

    Structures I University of Michigan, Taubman College Slide 7 of 31

    Method of Joints

    Method of Sections

    Graphic MethodsJames Clerk Maxwell 1869M. Williot 1877Otto Mohr 1887Heinrich Müller-Breslau 1904

    Computer ProgramsDr. Frame (2D)STAAD Pro (2D or 3D)West Point Bridge Designer

    Analysis

    James Clerk Maxwell

    Structures I University of Michigan, Taubman College Slide 8 of 31

  • 1. Solve reactions (all external forces)2. Inspect for zero force members (T’s & L’s)3. Cut FBD of one joint4. Show forces as orthogonal components5. Solve with FH and FV (no M)6. Find resultant member forces

    (Pythagorean Formula)

    Method of Joints – procedure

    Structures I University of Michigan, Taubman College Slide 9 of 31

    T – jointsL – joints

    Inspection of Zero Force Members

    Structures I University of Michigan, Taubman College Slide 10 of 31

  • 1. Solve the external reactions for the whole truss.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 11 of 31

    2. T or L joints by inspection.3. Cut FBD of joint4. Show orthogonal components5. Solve by F horz. and vert.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 12 of 31

  • Continue with joints having only one unknown in either horizontal or vertical direction. Generally work starting at the reactions.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 13 of 31

    Continue moving across the truss, joint by joint. Solve by FH and FV .

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 14 of 31

  • Continue moving across the truss, joint by joint. Choose joints that have only one unknown in each direction, horizontal or vertical.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 15 of 31

    Solve the joints with the most members last.Check that all forces balance.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 16 of 31

  • Inspect the final solution to see that it seems to make sense.

    Method of Joints - example

    Structures I University of Michigan, Taubman College Slide 17 of 31

    Qualitative T or C

    For typical gravity loading:(tension=red compression=blue)

    Top chords are in compression

    Bottom chords are in tension

    Diagonals down toward center are in tension (usually)

    Diagonals up toward center are in compression (usually)

    Structures I University of Michigan, Taubman College Slide 18 of 31

  • Qualitative ForceFor spanning trusses with uniform loading: (tension=blue compression=red)

    Top and bottom chords greatest at center when flat (at maximum curvature or moment)

    Diagonals greatest at ends (near reactions, i.e. greatest shear)

    Structures I University of Michigan, Taubman College Slide 19 of 31

    1. Solve Reactions

    2. Cut section through member

    3. Choose point where all but one of the unknown forces cross and M

    4. Continue with FH and FV

    Method of Sections - procedure

    Structures I University of Michigan, Taubman College Slide 20 of 31

  • 1. Solve the external reactions for the whole truss.

    Sum moments about each end. Or using symmetry, divide vertical forces evenly between reactions

    Structures I University of Michigan, Taubman College Slide 21 of 31

    Method of Sections - example

    2. Solution proceeds by cutting FBDs of either joints or sections of the truss.

    Member forces are shown as horizontal and vertical force components at each cut section.

    Structures I University of Michigan, Taubman College Slide 22 of 31

    Method of Sections - example

    75k 75k

  • 2. Solution proceeds by cutting FBDs of either joints or sections of the truss.Member forces are shown as horizontal and vertical force components at each cut section.

    3. Choose a point where all but one of the forces cross and sum moments.

    Structures I University of Michigan, Taubman College Slide 23 of 31

    Method of Sections - example

    75k 75k

    83.9k

    Structures I University of Michigan, Taubman College Slide 24 of 31

    4. Continue with FH and FV

    Member forces are shown as horizontal and vertical force components at each cut section.

    Method of Sections - example

    75k 75k

    83.9k

    80.3k

    37.5k

  • 4. Continue with FH and FV

    Member forces are shown as horizontal and vertical force components at each cut section.

    Structures I University of Michigan, Taubman College Slide 25 of 31

    Method of Sections - example

    75k 75k

    83.9k

    80.3k

    37.5k

    70.3k

    37.9k

    2. Solution proceeds by cutting FBDs of either joints or sections of the truss.Member forces are shown as horizontal and vertical force components at each cut section.

    3. Choose a point where all but one of the forces cross and sum moments.

    Structures I University of Michigan, Taubman College Slide 26 of 31

    Method of Sections - example

  • Structures I University of Michigan, Taubman College Slide 27 of 31

    4. Continue with FH and FV

    Member forces are shown as horizontal and vertical force components at each cut section.

    Method of Sections - example

    5. Make final qualitative check of solution.

    Structures I University of Michigan, Taubman College Slide 28 of 31

    Method of Sections - example

  • Howe Truss1. Cut a panel with diagonals

    M at L2 and resolve upper chord force at U2. This gives U1U2H

    M at U1 to find L1L2 M at U2 and resolve U1L2 at L2 to

    find U1L2H

    M at L0 and resolve U1L2 at L2 to find U1L2V

    6. U1U2V can now be found by FV

    Tips on Sections

    Structures I University of Michigan, Taubman College Slide 29 of 31

    Parker Truss

    1. Cut a panel with diagonals and M at L2 to solve U1U2H as before.

    M at U1 to find L1L2 M at U2 and resolve U1L2 at L2 to

    find U1L2H

    4. Find point x in line with U1U2. M at x and resolve U1L2 at L2 to find U1L2V

    5. U1U2V can now befound by FV

    Tips on Sections

    Structures I University of Michigan, Taubman College Slide 30 of 31

  • K Truss1. Make cut A-A to avoid the mid panel

    joint

    M at U1 to get L1L2 M at L1 to get U1U24. The vertical web forces can be

    solved using joints

    5. Cut B-B through the diagonals

    M at U2 and resolve lower diagonalat L2 to find its H component. The V component can be found by slope triangle. Top and bottom chords are known from steps 2. & 3.

    7. Repeat step 6 by M at L2 to find other diagonal.

    Tips on Sections

    Structures I University of Michigan, Taubman College Slide 31 of 31