Week 9 Challenge
SOLUTION 1
REFER STAAD MODEL STRUCTURE 50
GIVEN DATA
Bay spacing as 5 m
Frame width is 20 m
Slope of the roof is 1 in 10
LOADING DATA
Roof is accessible for maintenance purpose (assume 75 kg/m2)
Weight of roofing sheet = 5kg/m2
Weight of purlins + tertiary members = 25 kg/m2
DESIGN CODE
Design code as per AISC:ASD
ASSUMING HEIGHT OF THE COLUMN AS 10 M
Slope of the roof is 1 in 10
THETA=TAN^-1(1/10)=5.71
10*TAN(5.71)=0.999 =APPROX 1M
LOAD CALCULATION
DEAD LOAD
Weight of roofing sheet = 5kg/m2
Weight of purlins + tertiary members = 25 kg/m2
TOTAL DEAD LOAD =30 kg/m2 = 0.3 kN/m^2
UDL ON RAFTER=TOTAL LOAD*BAY SPACING=0.3*5=1.5 KN/M
LOAD CALCULATION
LIVE LOAD
Roof is accessible for maintenance purpose (assume 75 kg/m2)
TOTAL LIVE LOAD =75 kg/m2 = 0.75 kN/m^2
UDL ON RAFTER=TOTAL LOAD*BAY SPACING=0.75*5=3.75 KN/M
SUPPORT CONDITION
PINNED
STEP 1.
OPEN STAAD PRO
DEFINE GEOMETRY
BY PUTTING THE NODE DATA IN X,Y AND Z IN M

STEP 2
DEFINE MATERIAL
STEEL

STEP 3
DEFINE PROPERTY
TAPERED I

STEP 4.
DEFINE SUPPORT CONDITION
PINNED

STEP 5.
DEFINE LOAD
DEFINE LOAD CASE DETAILS
ADD
1 DEAD LOAD
DEFINE UNIFORM FORCE W1=-1.5 KN/M
DIRECTION =GY
2 LIVE LOAD
DEFINE UNIFORM FORCE W1=-3.75 KN/M
DIRECTION =GY
DEFINE LOAD COMBINATION
1DL+1 LL
LOAD FACTOR DL=1
LOAD FACTOR LL=1
ADD
APPLY BOTH LOAD ON RAFTER


GO TO ANALYSIS IN RIBBON TOOL BAR
DEFINE COMMAND
PERFORM ANALYSIS PRINT ALL
ADD
GO TO DESIGN IN RIBBON TOOL BAR
CHOOSE CURRENT CODE
AISC:ASD
CHOOSE
CHECK CODE
STEEL MEMBER TAKE OFF
ADD


RUN THE ANALYSIS
BENDING MOMENT DIAGRAM
MZ



BENDING MOMENT DIAGRAM
MY

SHEAR FORCE DIAGRAM
FZ


SHEAR FORCE DIAGRAM
FY


AXIAL FORCE DIAGRAM
FX


SOLUTION 2.
REFER STAAD MODEL CHALLENGE 41
FIGURE 1.
HEIGHT OF THE COLUMN IS 10 M
THETA=5.71
10*TAN(5.71)=0.999 =APPROX 1M
STEP 1.
OPEN STAAD PRO
DEFINE GEOMETRY
BY PUTTING THE NODE DATA IN X,Y AND Z IN M

STEP 2
DEFINE MATERIAL
STEEL

STEP 3
DEFINE PROPERTY
ISMB 400 FOR COLUMNS
ISMB 300 FOR BEAMS

STEP 4.
DEFINE SUPPORT CONDITION
PINNED FOR EXTERNAL COLUMN
FIXED FOR INTERNAL COLUMN

STEP 5.
DEFINE LOAD
DEFINE LOAD CASE DETAILS
ADD
1 DEAD LOAD
NODAL LOAD
NODE LOAD
FX =10 KN (APPLY TO NODE 4 )
FX=-10 KN (APPLY TO NODE 6 )


DEFINE UNIFORM FORCE W1=-20 KN/M
DIRECTION =GY
APPLY TO RAFTER

GO TO ANAYLSIS IN RIBBON TOOL BAR
ADD PERFORM ANALYSIS PRINT ALL
Draw Bending Moment diagram for following Frame using STAAD.Pro


BMD DIAGRAM WITH VALUES


FIGURE 2.
REFER STAAD MODEL STRUCTURE 51
HEIGHT OF THE COLUMN AT NODE 1 IS 16.36 M
HEIGHT OF THE COLUMN AT NODE 2 IS 20 M
THETA=20
10*TAN(20)=3.64 M
STEP 1.
OPEN STAAD PRO
DEFINE GEOMETRY
BY PUTTING THE NODE DATA IN X,Y AND Z IN M

STEP 2
DEFINE MATERIAL
STEEL

STEP 3
DEFINE PROPERTY
ISMB 600 FOR COLUMNS
ISMB 450 FOR BEAMS

STEP 4.
DEFINE SUPPORT CONDITION
PINNED FOR EXTERNAL COLUMN

STEP 5.
DEFINE LOAD
DEFINE LOAD CASE DETAILS
ADD
1 DEAD LOAD
NODAL LOAD
NODE LOAD
FX =30 KN (APPLY TO NODE 3 )

DEFINE UNIFORM FORCE W1=-10 KN/M
DIRECTION =GY
APPLY TO RAFTER

GO TO ANAYLSIS IN RIBBON TOOL BAR
ADD PERFORM ANALYSIS PRINT ALL
Draw Bending Moment diagram for following Frame using STAAD.Pro


BMD WITH VALUES


FIGURE 3
REFER STAAD MODEL STRUCTURE 56
HEIGHT OF THE COLUMN IS 10 M
STEP 1.
OPEN STAAD PRO
DEFINE GEOMETRY
BY PUTTING THE NODE DATA IN X,Y AND Z IN M

STEP 2
DEFINE MATERIAL
STEEL

STEP 3
DEFINE PROPERTY
ISMB 500 FOR COLUMNS
ISMB 350 FOR BEAMS

STEP 4.
DEFINE SUPPORT CONDITION
PINNED FOR EXTERNAL COLUMN

STEP 5.
DEFINE LOAD
DEFINE LOAD CASE DETAILS
ADD
1 DEAD LOAD
DEFINE UNIFORM FORCE W1=2 KN/M
DIRECTION =GX
APPLY TO LEFT COLUMN

1 DEAD LOAD
GO TO MEMBER LOAD
DEFINE CONCENTRATED FORCE P= -10 KN
DIRECTION =GY
APPLY TO BEAM

GO TO ANAYLSIS IN RIBBON TOOL BAR
ADD PERFORM ANALYSIS PRINT ALL
Draw Bending Moment diagram for following Frame using STAAD.Pro


BMD WITH VALUES


SOLUTION 3.
3. Deflection of a frame, present result from STAAD.Pro
Determine the lateral deflection at point A & Vertical deflection at mid section of beam between B & C from Figure 1 in previous challenge.
Lateral deflection at point A =NODE 4


Vertical deflection at mid section of beam between B & C
X DIRECTION

Y DIRECTION

Determine the lateral deflection at point A & Vertical deflection at mid section of beam between A & B from Figure 2 in previous challenge.
lateral deflection at point A = NODE 3


Vertical deflection at mid section of beam between A & B
X DIRECTION

Y DIRECTION

Determine the lateral deflection at point A & point B from Figure 3 in previous challenge
LATERAL DEFLECTION AT PONT A = NODE 1 AND POINT B =NODE 3

LATERAL DEFLECTION AT PONT B= NODE 3

LATERAL DEFLECTION AT PONT A = NODE 1
