RESPONSE 2000
RESPONSE 2000 Copyright Evan Bentz and Michael P. Collins,
September 2001
PresentationTopic: Response 2000
Subject: Prestressed Concrete Structures
Prepared by: Sufian AhmadDate: 13th April, 2015
Response 2000Introduction:
This program is based on the latest research ofModified
Compression Field Theory
And is developed at theUniversity of Toronto by Evan Bentz in a
project supervised by Professor Michael P. Collins
Download Link: http://www.ecf.utoronto.ca/~bentz/r2k.htm
Response-2000
Response 2000Introduction:
It is a Sectional Analysis Program
used to Predict the Load Deformation response
of Reinforced/Prestressed concrete sections
subjected to combined actions of Shear, Moment and Axial
load
Response 2000Introduction:Applicability of sectional
analysis
Beam theory assumes that response of a section depends only on
The section properties Values of applied stresses resultants
It ignores the details of how the forces are introduced in
members
Response 2000Introduction:Applicability of sectional
analysis
St. Venant's PrincipleB regions: Beam actionD regions: Arch
action
Response 2000
Response 2000Interface:
Response 2000Interface:
Components of each menu item.
FileDefineLoadsSolveViewOptionsHelpNew Open Close Save Save
AsPrint Preview PrintPrint Setup MRU List ExitQuick Define Edit
GeneralMaterial Properties Concrete Section Transverse
Reinf.LoadsTime Dep. Effects Detail T&S Strains Strain
DiscontinuityFull Member PropertiesFull-Response More-Detail Member
Response One Load2-Strain 1-StrainM-N Interaction M-V Interaction
N-V Interaction Stop AnalysisCross Section1 Cross Section Plot9
Cross Section Plots Next Load Stage Previous Load
StageLoad-Deformation PlotPushover ResultsPreferences Print in
Color Object Options Insert Text BoxInsert Beam Graphic Insert
ChartDelect SelectionContents Using Help AboutLongitudinal
Reinf.Tendons Response 2000Example 1:
See the response of member A subjected to axial tension.
Response 2000Example 1:Results and Discussion
Member A
As = 2.48sq-in11 Response 2000Example 2:
See the response of member C subjected to axial tension.
12 Response 2000Example 2:
13 Response 2000Example 2:
14 Response 2000Presentation of results:
