F 26 2 C S X 2 B A solid bar S (E-200 GPa, A=100 mm²) is attached to a cantilever beam (E-200 GPa, 1=250*106 mm) as shown in the figure. Calculate the force S in the bar due to an applied force F=100 kN at the free end of the cantilever. Disregard axial deformations of the beam. a=30°, L=4m

F 26 2 C S X 2 B A solid bar S (E-200 GPa, A=100 mm²) is attached to a cantilever beam (E-200 GPa, 1=250*106 mm) as shown in the figure. Calculate the force S in the bar due to an applied force F=100 kN at the free end of the cantilever. Disregard axial deformations of the beam. a=30°, L=4m

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

Determine the maximum tensile and compressive bending stresses developed in the beam shown. The cross-section has the given properties. NA 1-35 x 10mm a. RA = b. RE= c. fb(c) = d. fb(T) = 80 mm 200 mm A 1.5m kN KN 5kN m MPa MPa B 1.5m SkN/m 2m 5KN n 2m 4
An aluminum bar having a cross-sectional area of 160 mm? carries the axial loads as shown in the Figure below. Assume that the bar is suitably braced to prevent buckling and E = 70000 MPa. The length of each bars are follow: B, = 0.8 m; B, = 1.0 m; B3= 0.6 m. Determine the axial load acting on bar Bị in kN. 35KN В1 B2 ВЗ ... 10KN 15KN 30KN Determine the axial load acting on bar B2 in kN. Determine the axial load acting on bar B3 in kN. Determine the axial stress of bar B1 in MPa. Determine the axial stress of bar B2 in MPa. Determine the axial stress of bar B3 in MPa. Determine the total deformation of the bars B1, B2 and B3 in mm. Determine the deformation of the bar B in mm. Determine the deformation of the bar B2 in mm. Determine the deformation of the bar Bz in mm. 35 А 35 B 20 10
P5 The pin-connected structure shown in the figure consists of a rigid beam ABCD and two supporting bars. Bar AE is an aluminium alloy [EAE 70 GPa] with a cross-sectional area of AAE = 2,400 mm². Bar CF is a bronze alloy [ECF = 100 GPa] with a cross-sectional area of ACF = 6,000 mm². A downward load P=298 kN is applied at point B. Determine the normal stress created in bras AE and CF. E 2.9 m 0.8 m B P 1.5 m 3.3 m 1.2 m D
An axial member consisting of two polymer bars is supported at C as shown. Bar (1) has a cross-sectional area of 680 mm² and an elastic modulus of 29 GPa. Bar (2) has a cross-sectional area of 1580 mm² and an elastic modulus of 15.2 GPa. Determine the deflection of point A relative to support C. 70 KN 0.85 m O -1.902 mm O-2.101 mm O -2.250 mm O-1.354 mm O -2.879 mm 90 kN (1) 90 kN B (2) 1.15 m
A:Y 211O 2_531929016114... -> A rod is composed of an aluminum section rigidly attached between steel and bronze sections, as shown in Figure below. Axial loads are applied at the positions indicated. If P = 11 KN and the cross sectional area of each rod is 312.5 mm, determine the stress in each section. 4P Steel Bronze |Aluminum 609.6 mm 914.4 mm 762 mm
A rigid bar AB, pinned at end A, is supported by a wire CD and loaded by a force P end B as shown in figure. The wire is made of high- strength steel having modulus of elasticity E= 210 GPa. The diameter of the wire is 5mm. Determine the maximum load P that could be applied so that the vetical displacemt at B will not be more than 6 mm?
Compute the maximum tensile and comprsive stresses devloped in the beam that is loaded and has the cross-sectional properties shown in fig 8 KN 120 mm 10 KN/m ΝΑ A 1=20 x10 6 mm4 4m B C 1m 50 mm
The Figure below shows a two-member truss supporting a block of weight W. The cross-sectional areas of the members are 800 mm² for AB and 400 mm² for AC. Determine the maximum safe value of W (kN) if the working stresses are 110 MPa for AB and 120 MPa for AC. ... B 40 deg. A 60 deg. A) 38.90 в) 55.30 61.70 76.2
The rigid bar BDE is supported by two links AB and CD. Link AB is made of aluminum (E = 70 GPa) and has a cross-sectional area of 519 mm2; link CE is made of steel (E = 200 GPa) and has a cross-sectional area of 619 mm?. For the 41 kN force shown, determine the deflection of B (mm) *deflection should have a negative sign if compression and positive if tension. Also, your final answer should have two decimal places 04 m 0.3 m E 0.4 m 0.2 m
The rigid bar BDE is supported by two links AB and CD. Link AB is made of aluminum (E = 70 GPa) and has a cross-sectional area of 519 mm2; link CE is made of steel (E = 200 GPa) and has a cross-sectional area of 633 mm2. For the 36 kN force shown, determine the deflection of B (mm) *deflection should have a negative sign if compression and positive if tension. Also, your final answer should have two decimal places
3. The rigid bar BDE is supported by two links AB and CD. Link AB is made of steel (E=200 GPa) and has a cross-sectional area of 700 mm'; link CD is made of aluminum (E=70 GPa) and has a cross sectional area of 500 mm. For the 28 kN force shown, deflection at E. A 0.4 m 0.3 m 28 kN D 0.25 m 0.60 m
Q1/ A thin-walled cantilever has a constant cross-section of uniform thickness with the dimensions shown in Figure. It is subjected to a system of point loads acting in the planes of the walls of the section in the directions shown. Calculate the direct stresses according to the basic theory of bending at the points 1,2 and 3 of the cross-section at the built-in end along the beam. 50N 2 mm 50 N 80N 2 mm 100 mm 2 36 mm 80 mm 24 mm