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Method of Sections, Lecture notes of Engineering

METHOD OF SECTIONS. Learning Objectives. 1). To employ the method of sections to evaluate the axial force carried by selected members in a truss.

Typology: Lecture notes

2021/2022

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METHOD OF SECTIONS
Learning Objectives
1). To employ the method of sections to evaluate the axial force
carried by selected members in a truss.
2). To do an engineering estimate of the load in select members
of a truss.
Procedure
1). Draw a FBD of the entire truss showing the reaction forces
at the supports and the external loads. Write the
equilibrium equations and solve for as many unknowns as
possible.
2). Locate the force members to be evaluated. Identify whether
any of these forces can be determined by observation (e.g.,
zero-force members).
3). Identify section to be used and draw a FBD of the section
including any support reactions, external loads and internal
forces of sectioned members. Remember, the cutting plane
must cut through the members of interest. Also the cutting
plane need not be straight, it may be curved.
4). Write the equilibrium equations for one of the two sections.
The equations for either half of the section will yield the
same member forces.
5). Three equilibrium equations are available, so up to three
unknowns can be solved with a single section.
6). At times more than one section may be necessary.
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METHOD OF SECTIONS

Learning Objectives

1). To employ the method of sections to evaluate the axial force

carried by selected members in a truss.

2). To do an engineering estimate of the load in select members

of a truss.

Procedure

1). Draw a FBD of the entire truss showing the reaction forces

at the supports and the external loads. Write the

equilibrium equations and solve for as many unknowns as

possible.

2). Locate the force members to be evaluated. Identify whether

any of these forces can be determined by observation (e.g.,

zero-force members).

3). Identify section to be used and draw a FBD of the section

including any support reactions, external loads and internal

forces of sectioned members. Remember, the cutting plane

must cut through the members of interest. Also the cutting

plane need not be straight, it may be curved.

4). Write the equilibrium equations for one of the two sections.

The equations for either half of the section will yield the

same member forces.

5). Three equilibrium equations are available, so up to three

unknowns can be solved with a single section.

6). At times more than one section may be necessary.

Method of Sections

Example 1

Given: Truss A-M is supported by a pin support at joint A and a roller support at joint M. The truss is loaded with two 15kip forces as shown. (Note: 1kip = 1,000lbs.)

Find:

a) Determine the reaction forces at supports A and M.

b) By inspection, identify all zero-force members in the truss. What else can you determine about the truss by inspection?

c) Using the method of sections, determine the loads in members DE, KL, and DK. State whether each of these members are in tension or compression.

Method of Sections

Example 2

Given: The overhead sign truss shown is a K-truss which is supported by a pin joint at U and a rocker support at V. The truss is loaded with these forces as shown and is in static equilibrium.

Find:

a) Determine the reactions at supports U and V.

b) Determine the loads in members DE, DR, KR, and JK. State whether each member is in tension or compression.