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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

Plane Trusses - structures1.tcaup.umich.eduPlane Trusses Definition and Assumptions Nomenclature Stability and Determinacy Analysis by joints Analysis by sections Analysis and design

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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

Panels

Joints• 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) Stable

B) 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 joint

4. Show forces as orthogonal components

5. 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 – joints

L – 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 joint

4. Show orthogonal components

5. 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 Force

For 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 Truss

1. 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 Truss

1. Make cut A-A to avoid the mid panel joint

M at U1 to get L1L2

M at L1 to get U1U2

4. The vertical web forces can be solved using joints

5. Cut B-B through the diagonals

M at U2 and resolve lower diagonal

at 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