All of the statements are correct except Select the correct response In a cantilever beam, the tangential deviation of a point along the beam from a tangent drawn from the fixed support will equal the deflection at that point. The deviation of any point B relative to a tangent drawn to the elastic curve at any other point A, in a direction perpendicular to the original position of the beam, is equal to the product 1/El multiplied by the moment of area about B of that part of the moment diagram between points A and B. The resultant bending moment at any section caused by any load system is the algebraic sum of the bending moments at that section caused by each load acting separately. none of these

All of the statements are correct except Select the correct response In a cantilever beam, the tangential deviation of a point along the beam from a tangent drawn from the fixed support will equal the deflection at that point. The deviation of any point B relative to a tangent drawn to the elastic curve at any other point A, in a direction perpendicular to the original position of the beam, is equal to the product 1/El multiplied by the moment of area about B of that part of the moment diagram between points A and B. The resultant bending moment at any section caused by any load system is the algebraic sum of the bending moments at that section caused by each load acting separately. none of these

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

I need help on this question: a) Find the value of the integration constant C4. The answer should be in kNm2 to three decimal places. b) Find the value of the deflection at point C. The answer should be in mm to three decimal places.
A rigid bar AB is loaded as shown in fig. What is the deflection of point B of the bar AB?
Using Double Integration Method Calculate the deflection at the free end of the beam shown below.
a) Using Macauley's Method, calculate a general expression in terms of Young's Modulus, E, and Second Moment of Area, I, for the deflection in the beam shown in Fig. 4.1. R₁ 4kN 32kNm 4m 4m → 4m pesadas Figure 4.1 20 1kN/m 150 R₂ Figure 4.2 (All dimensions in mm) 4m If the beam in part a) has the cross-sectional profile as shown below and a Young's Modulus, E, of 200GN/m², calculate the magnitude of the deflection at 10m from the left hand side. 4kN ➜
Determine the slope and deflection at point A of the beam shown in figure below by conjugate beam method
a) Using Macauley's Method, calculate a general expression in terms of Young's Modulus, E, and Second Moment of Area, I, for the deflection in the beam shown in Fig. 4.1. R₁ 300N 0.4m 0.4m 200N/m 55 0.4m Figure 4.1 If the beam in part a) has the cross-sectional profile as shown below and a Young's Modulus, E, of 70GN/m², calculate the magnitude of the deflection at 1.1m from the left hand side. 0.4m 0.4m 15 25Nm H A R₂ [10 40 Figure 4.2 (All dimensions in mm, wall thickness is 5mm) What is the value of stress at point A in Fig. 4.2 at a point 1.1m from the left hand side of the beam?
Using Double Integration Method calculate the deflection at the free end of the beam.
Determine the maximum deflection using conjugate beam method of the shown beam.
Create a non prismatic beam figure and using Area moment method, find the location and magnitude of maximum deflection in a non-prismatic beam.
And do g) the value of the deflection at point C in mm to three decimal points
Using double integration method, determine the maximum deflection of the beam shown. (Hint: utilize symmetry, analyze only right half of the beam.) w w В L/2 L/2
If the deflection at the free end of a uniformly loaded cantilever beam is 15 mm and the slope of the deflection curve at the free end is 0.02 radian, then the length of the beam is..