The beam is subjected to the distributed loads shown and supported by a rocker at C and a pin at A. Point D is located halfway between A and B. Point E is located halfway between B and C. A. Draw both FBDs (above and below cut) you could use to solve for the internal axial force (AD), shear force (VD), and bending moment (MD) at point D. B. Draw both FBDs (left and right of cut) you could use to solve for the internal axial force (AE), shear force (VE), and bending moment (ME) at point E. Ensure all internal loads (A, V, & M) on FBDs are drawn in the assumed positive direction. Represent distributed loads as equivalent point forces. You do not need to solve for internal loads, just draw the FBDs. 200 N/m 200 N/m B 5 m E 6 m 100 N/m C

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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The beam is subjected to the distributed loads shown and
supported by a rocker at C and a pin at A. Point D is located
halfway between A and B. Point E is located halfway
between B and C.
A. Draw both FBDs (above and below cut) you could use
to solve for the internal axial force (AD), shear force
(VD), and bending moment (MD) at point D.
B. Draw both FBDs (left and right of cut) you could use to
solve for the internal axial force (AE), shear force (VE),
and bending moment (ME) at point E.
Ensure all internal loads (A, V, & M) on FBDs are drawn in
the assumed positive direction. Represent distributed loads
as equivalent point forces. You do not need to solve for
internal loads, just draw the FBDs.
200 N/m
200 N/m
B
5 m
E
6 m
100 N/m
C
Transcribed Image Text:The beam is subjected to the distributed loads shown and supported by a rocker at C and a pin at A. Point D is located halfway between A and B. Point E is located halfway between B and C. A. Draw both FBDs (above and below cut) you could use to solve for the internal axial force (AD), shear force (VD), and bending moment (MD) at point D. B. Draw both FBDs (left and right of cut) you could use to solve for the internal axial force (AE), shear force (VE), and bending moment (ME) at point E. Ensure all internal loads (A, V, & M) on FBDs are drawn in the assumed positive direction. Represent distributed loads as equivalent point forces. You do not need to solve for internal loads, just draw the FBDs. 200 N/m 200 N/m B 5 m E 6 m 100 N/m C
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