Moment (KN.m)3002502001501005000AMoment-Curvature Relation0.01 0.02 0.03 0.04 0.05 0.06 0.07Curvature (1/m)Lb) Yield displacement (Ay).Ay=Calculate the following values:a) Yield Force (Fy) that will cause the system to yield at point A.Fy=c) Plastic displacement (Ap).Ap=Hint: Au Ap+Ay=Başka yönergeler almak için tıklayınFor the cantilever beam system given, construct the relation between the force (F) and the displacement (A) of the free end. You need to transform the moment curvature relation given into force-displacement relation.Beam length: L = 3.5 mPlastic hinge length: Lp = 0.3 mNote: All the results are positive.Fe) The ultimate (failure) force (Fu)Fu =d) Ultimate (failure) displacement (Au).Au=(m)0.08 0.09(m)FAhaAyAu(KN) (Write 2 digits after the decimal point)(m) (Write 4 digits after the decimal point)(Write 4 digits after the decimal point)(Write 4 digits after the decimal point)A(KN) (Write 2 digits after the decimal point)

A cantilever beam with point load, F and moment curvature relationLength of the beam, L =3.5 mLength…

Calculate the following values: a) Yield Force (Fy) that will cause the system to yield at point A. Fy= b) Yield displacement (Ay). Ay= c) Plastic displacement (Ap). Ap= (KN) (Write 2 digits after the decimal point) (m) (Write 4 digits after the decimal point) (m) (Write 4 digits after the decimal point) d) Ultimate (failure) displacement (Au). Au= (m) Hint: Au= Ap+Ay e) The ultimate (failure) force (Fu) Fu= (Write 4 digits after the decimal point) (KN) (Write 2 digits after the decimal point)

Calculate the following values: a) Yield Force (Fy) that will cause the system to yield at point A. Fy= b) Yield displacement (Ay). Ay= c) Plastic displacement (Ap). Ap= (KN) (Write 2 digits after the decimal point) (m) (Write 4 digits after the decimal point) (m) (Write 4 digits after the decimal point) d) Ultimate (failure) displacement (Au). Au= (m) Hint: Au= Ap+Ay e) The ultimate (failure) force (Fu) Fu= (Write 4 digits after the decimal point) (KN) (Write 2 digits after the decimal point)

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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