Challenge

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

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