Piña_Carga_Muerta

8/3/2019 Pia_Carga_Muerta

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==========================S T R A N -- Version 4.0==========================

Copyright 1998 by Russell C. Hibbeler

The output from this program is to be used for academic andeducational purposes only, and is not for professional use.

Problem Title: Marco de un nivel y dos claros

Structure Type: PLANE FRAME

********************* NODE COORDINATES *********************

Node No. 1:X-Coordinate = 0Y-Coordinate = 0


Node No. 3:X-Coordinate = 1600

Y-Coordinate = 0




********************** MEMBER PROPERTIES **********************

Member No. 1:Near Node = 1Far Node = 4Youngs Modulus = 249229Section Area = 2500Moment of Inertia = 520833.33Near Moment Released = NoFar Moment Released = No

Member No. 2:

Near Node = 2Far Node = 5Youngs Modulus = 249229Section Area = 2500Moment of Inertia = 520833.33Near Moment Released = NoFar Moment Released = No


Member No. 4:Near Node = 4


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Far Node = 5Youngs Modulus = 249229Section Area = 2550Moment of Inertia = 1535312.5Near Moment Released = NoFar Moment Released = No


*********************** STRUCTURE SUPPORTS ***********************

Support at node no. 1:Restrained in X-direction, Support displacement = 0Restrained in Y-direction, Support displacement = 0Restrained in Rot-direction, Support displacement = 0

Support at node no. 2:Restrained in X-direction, Support displacement = 0Restrained in Y-direction, Support displacement = 0

Restrained in Rot-direction, Support displacement = 0

Support at node no. 3:Restrained in X-direction, Support displacement = 0Restrained in Y-direction, Support displacement = 0Restrained in Rot-direction, Support displacement = 0

********************************** APPLIED LOADINGS ON STRUCTURE **********************************

Distributed load on member no. 4:Algebraic value of load closest to

near node in member y' direction = -50Distance from near node = 0Algebraic value of load farthest fromnear node in member y' direction = -50Distance from near node = 800

Distributed load on member no. 5:Algebraic value of load closest tonear node in member y' direction = -45Distance from near node = 0Algebraic value of load farthest fromnear node in member y' direction = -45Distance from near node = 800

Concentrated force on member no. 5:Algebraic value in member y' direction = -6000Distance from near node = 400

************************************************* MEMBER END DISPLACEMENTS IN GLOBAL DIRECTION *************************************************

Member No. 1:Near end X-displacement = 0Near end Y-displacement = 0Near end Rot-displacement = 0Far end X-displacement = -1.90679028237023E-04Far end Y-displacement = -1.08389568679209E-02Far end Rot-displacement = -8.24055836771399E-04

Member No. 2:Near end X-displacement = 0


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Near end Y-displacement = 0Near end Rot-displacement = 0Far end X-displacement = -5.24588262279906E-03Far end Y-displacement = -3.03010098412802E-02Far end Rot-displacement = -9.33216568352368E-05

Member No. 3:Near end X-displacement = 0Near end Y-displacement = 0Near end Rot-displacement = 0Far end X-displacement = -1.10336295334402E-02Far end Y-displacement = -1.15023822951283E-02Far end Rot-displacement = 9.99728449529017E-04

Member No. 4:

Near end X-displacement = -1.90679028237023E-04Near end Y-displacement = -1.08389568679209E-02Near end Rot-displacement = -8.24055836771399E-04Far end X-displacement = -5.24588262279906E-03Far end Y-displacement = -3.03010098412802E-02Far end Rot-displacement = -9.33216568352368E-05

Member No. 5:Near end X-displacement = -5.24588262279906E-03Near end Y-displacement = -3.03010098412802E-02Near end Rot-displacement = -9.33216568352368E-05Far end X-displacement = -1.10336295334402E-02Far end Y-displacement = -1.15023822951283E-02Far end Rot-displacement = 9.99728449529017E-04

******************************** STRUCTURE SUPPORT REACTIONS ********************************

Support at node no. 1:X-direction support reaction = 4015.94188563276Y-direction support reaction = 16883.6398827192Rot-direction support reaction = -535768.310943902

Support at node no. 2:X-direction support reaction = 581.945184017293Y-direction support reaction = 47199.3148858276Rot-direction support reaction = -86104.5796907826

Support at node no. 3:X-direction support reaction = -4597.88706965006Y-direction support reaction = 17917.0452314532Rot-direction support reaction = 595148.611647414

******************************************************** MEMBER END FORCES IN LOCAL MEMBER COORDINATE SYSTEM ********************************************************

Member No. 1:Near end axial force = 16883.6398827192Near end shear force = -4015.94188563276Near end moment = -535768.310943902Far end axial force = -16883.6398827192Far end shear force = 4015.94188563276Far end moment = -1070608.4433092

Member No. 2:Near end axial force = 47199.3148858276Near end shear force = -581.945184017293Near end moment = -86104.5796907826Far end axial force = -47199.3148858276Far end shear force = 581.945184017293Far end moment = -146673.493916134

Member No. 3:Near end axial force = 17917.0452314532Near end shear force = 4597.88706965006

Near end moment = 595148.611647414Far end axial force = -17917.0452314532Far end shear force = -4597.88706965006


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Far end moment = 1244006.21621261

Member No. 4:Near end axial force = 4015.94188563276Near end shear force = 16883.6398827192Near end moment = 1070608.4433092Far end axial force = -4015.94188563276Far end shear force = 23116.3601172808Far end moment = -3563696.53713388

Member No. 5:Near end axial force = 4597.88706965006Near end shear force = 24082.9547685468Near end moment = 3710370.03105001Far end axial force = -4597.88706965006

Far end shear force = 17917.0452314532Far end moment = -1244006.21621261

Piña_Carga_Muerta

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