2) A beam loaded with both transverse and longitudinal loads as shown. This beam loading is typical of interior beams in an airplane fuselage which support all kinds of fixed equipment. Draw the axial loads, shear, and bending-moment diagram. 200 lb 4 1.8" G 600 lb "1 4' 2" 10007b 4" a 5" 5 1560 lb 12 i D 10" N B in E 2" 600
2) A beam loaded with both transverse and longitudinal loads as shown. This beam loading is typical of interior beams in an airplane fuselage which support all kinds of fixed equipment. Draw the axial loads, shear, and bending-moment diagram. 200 lb 4 1.8" G 600 lb "1 4' 2" 10007b 4" a 5" 5 1560 lb 12 i D 10" N B in E 2" 600
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![200 lb
2) A beam loaded with both transverse and longitudinal loads as shown.
This beam loading is typical of interior beams in an airplane fuselage
which support all kinds of fixed equipment. Draw the axial loads,
shear, and bending-moment diagram.
1.8"
G
600 lb
2"
100076
F
5"
40mm
FIG. I
5"
:
C
FIG. 2
1560 lb
12
1
7"
D
10"
2'
B
10
T
5"
600 lb](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F0cb20104-1b3c-4502-bcb6-c726057f419c%2Fd73b44ad-b3fc-4eab-93b0-287db44db43f%2F91pwzsc_processed.jpeg&w=3840&q=75)
Transcribed Image Text:200 lb
2) A beam loaded with both transverse and longitudinal loads as shown.
This beam loading is typical of interior beams in an airplane fuselage
which support all kinds of fixed equipment. Draw the axial loads,
shear, and bending-moment diagram.
1.8"
G
600 lb
2"
100076
F
5"
40mm
FIG. I
5"
:
C
FIG. 2
1560 lb
12
1
7"
D
10"
2'
B
10
T
5"
600 lb
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Step 1: Introducing given data
VIEWStep 2: Resolving forces at G & F about center of beam
VIEWStep 3: Resolving forces at C & D about center of beam
VIEWStep 4: Resolving forces at E about center of beam
VIEWStep 5: Draw FBD of beam & calculate reactions
VIEWStep 6: Shear force calculation
VIEWStep 7: Axial force calculation
VIEWStep 8: Bending moment calculation
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