Problem 1. The indeterminate frame shown below is loaded with lateral forces applied on each level. Using Factor Method, draw the approximate moment and shear diagram of the structure due to the applied loads. Show your complete solution from the determination of girder/column factor, carry over factor, girder/column moment factor up to computation of end-moment for each member. From your computation, provide the following unknowns in the Form; Girder factor at joint D, go Column factor at joint K, b. Girder moment factor at joint F, G, d. Column moment factor at joint E, C e. Bending moment at column AC, Mac f. Bending moment at girder ED, MD Bending moment at girder CD, Mo h. Bending moment at column HL, M Shear at column DG, Vos Shear at beam HI, M а KN 21 a=42kN d=4.20m b=48kN e=4.70m c=22kN f=4.00m 41 31 g=4.40m b KN C 21 31 41 31 51 c KN F 21 31 21 41 31 51 41 fm gm fm em d m dm
Problem 1. The indeterminate frame shown below is loaded with lateral forces applied on each level. Using Factor Method, draw the approximate moment and shear diagram of the structure due to the applied loads. Show your complete solution from the determination of girder/column factor, carry over factor, girder/column moment factor up to computation of end-moment for each member. From your computation, provide the following unknowns in the Form; Girder factor at joint D, go Column factor at joint K, b. Girder moment factor at joint F, G, d. Column moment factor at joint E, C e. Bending moment at column AC, Mac f. Bending moment at girder ED, MD Bending moment at girder CD, Mo h. Bending moment at column HL, M Shear at column DG, Vos Shear at beam HI, M а KN 21 a=42kN d=4.20m b=48kN e=4.70m c=22kN f=4.00m 41 31 g=4.40m b KN C 21 31 41 31 51 c KN F 21 31 21 41 31 51 41 fm gm fm em d m dm
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
The indeterminate frame shown below is loaded with lateral forces applied on each level.
Using Factor Method, draw the approximate moment and shear diagram of the structure due to the
applied loads. Show your complete solution from the determination of girder/column factor, carry over
factor, girder/column moment factor up to computation of end-moment for each member.
![Problem 1. The indeterminate frame shown below is loaded with lateral forces applied on each level.
Using Factor Method, draw the approximate moment and shear diagram of the structure due to the
applied loads. Show your complete solution from the determination of girder/column factor, carry over
factor, girder/column moment factor up to computation of end-moment for each member.
From your computation, provide the following unknowns in the Form;
Girder factor at joint D, go
b.
Column factor at joint K, C
Girder moment factor at joint F, G,
d.
Column moment factor at joint E, C
Bending moment at column AC, MAC
f.
Bending moment at girder ED, MID
Bending moment at girder CD, Mco
h.
Bending moment at column HL, M
Shear at column DG, Voa
Shear at beam HI, M.
a KN
21
a=42kN
d=4.20m
b=48kN
e=4.70m
41
c=22kN
31
f=4.00m
g=4.40m
b KN
21
31
E
41
31
51
с KN
F
21
G
31
H
21
41
31
51
41
K
fm
g m
fm
e m
d m
dm](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F1fe15103-fe91-4703-b3be-af7f8e61417f%2F0db9b2eb-2a9e-497f-ac43-289d2de778dd%2Fdv7epgx_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Problem 1. The indeterminate frame shown below is loaded with lateral forces applied on each level.
Using Factor Method, draw the approximate moment and shear diagram of the structure due to the
applied loads. Show your complete solution from the determination of girder/column factor, carry over
factor, girder/column moment factor up to computation of end-moment for each member.
From your computation, provide the following unknowns in the Form;
Girder factor at joint D, go
b.
Column factor at joint K, C
Girder moment factor at joint F, G,
d.
Column moment factor at joint E, C
Bending moment at column AC, MAC
f.
Bending moment at girder ED, MID
Bending moment at girder CD, Mco
h.
Bending moment at column HL, M
Shear at column DG, Voa
Shear at beam HI, M.
a KN
21
a=42kN
d=4.20m
b=48kN
e=4.70m
41
c=22kN
31
f=4.00m
g=4.40m
b KN
21
31
E
41
31
51
с KN
F
21
G
31
H
21
41
31
51
41
K
fm
g m
fm
e m
d m
dm
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