I need help with some parts of my homework , I require every part to be answered clearly as my worksheet is on my phone so might be a bit blurry. (b)Using the provided data:cross-section width w = 14 mm,cross-section hight h = 90 mm,length of the beam L =2 m,beam material's Young's modulus Q =225 GPa,applied bending moment MB = 8 kN.mThe value of the deflection at Point B caused by MB (Part I) can be calculated as●●●give the answer in mm for the deflection at point B caused by MB(c)Based on the given values of dimensions and material parameters,the value of R can be calculated askN;the value of the vertical reaction force at Support A can be calculated asthe value of the horizontal reaction force at Support A can be calculated asthe absolute value of the reaction moment at Support A can be calculated askN;KNkN.m BA propped cantilever beam is loaded by a bending moment of the magnitude M³ at the point B asshown in Figure Q1. The cross-section of the beam is a rectangle of the width w and the hight hthat are constant along the length of the beam L. The beam material's Young's modulus is Q.AYOBMeBXFigure Q1Assuming the positive deflections and positive vertical reaction forces are upward, calculatethe value of the reaction forces at points A and Bthe absolute value of the reaction bending moment at point A

Answered: Image /qna-images/answer/6ef8731c-99b2-495b-b3d6-d7a2b34f53ae.jpg

A propped cantilever beam is loaded by a bending moment of the magnitude MB at the point B as shown in Figure Q1. The cross-section of the beam is a rectangle of the width w and the hight h that are constant along the length of the beam L. The beam material's Young's modulus is Q. |- O X Figure Q1 Assuming the positive deflections and positive vertical reaction forces are upward, calculate the value of the reaction forces at points A and B O the absolute value of the reaction bending moment at point A

A propped cantilever beam is loaded by a bending moment of the magnitude MB at the point B as shown in Figure Q1. The cross-section of the beam is a rectangle of the width w and the hight h that are constant along the length of the beam L. The beam material's Young's modulus is Q. |- O X Figure Q1 Assuming the positive deflections and positive vertical reaction forces are upward, calculate the value of the reaction forces at points A and B O the absolute value of the reaction bending moment at point A

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

The beam ABC is subjected to a point load at the middle of segment AB and a uniformly distributed load at the segment BC, as shown in the figure. A 20 N Set Wo B 1.5W, N/m H Figure 1: Overhang beam L C Find the maximum absolute value of the deflection between the supports A and B - 3 N/m, L = 2 m, EI = 25000 Nm². Use the method of superposition for all parts. Hint: for x > L/2 in segment AB, the solution can be obtained from the table by replacing x by L-x.
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 500 mm; link CD is-made of steet E = 200 GPa) and has a cross-sectional area 600 mm. For the 30-kN force shown, determine the deflection (a) of B, (b) of D, (c) of E. 0.4 m 0.3 m 30 kN E T0.4 m 0.2 m
In the restrained beam shown, solve for the following a. end moments b. max deflection 15KN im
Analyze the loaded beam as shown. Be guided as follows: Solve for the reactions at supports Draw Shear and Moment Diagrams Compute for deflection at A (AA) and slope at C (0c) using Conjugate Beam Method a. b. С. 50 kN 90 kN D A C 6 m 9 m 9 m El = constant E = 70 GPa %3D I = 95 (106) mm4
The load on a cantilever beam AB has a triangular distribution with maximum intensity ^(see figure). Determine the angle rotation BB and the deflection SB at the free end.
QUESTION 03 A beam ABCD is supported and loaded as shown in Figure Q3. The flexural rigidity, El is constant. By using Macaulay's method, and take point A as origin, determine the: (a) Reactions at all supports A, C and D. (b) Deflection at point B (c) Slope at support A 1 m 1 m 1 m 2 kN/m 4 kNm Figure Q3/ Rajah S3
i. For the beam shown in Figure assume that EI = 100,000 kip-fi? and use discontinuity functions to determine (a) the reactions at A, C, and D. (b) the beam deflection at B. 75 kips
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 500 mm^2; link CD is made of steel (E = 200 GPa) and has a cross-sectional area of 600 mm^2. For the 30 kN force shown, determine the deflection of B and E, respectively. 0.4 m 0.3 m B A 0.2 m OC -0.4 m 30 kN E
B.2. Elementary beam theory predicts that the axial bending stress ox in a prismatic beam is given by: σ, X (M.1, M,1,)y+ (M, I. - M.1,-) z (1,1.-1²-) where My and M₂ are bending moments applied to a cross-section, and where ly, Iz and lyz are second moments of area in the usual notation (Oxyz is a Cartesian coordinate system in which the x axis corresponds to the centroidal axis of the beam). (i) What assumptions have been made in the derivation of the above expression? (ii) Indicate by means of a sketch the directions in which positive values of the bending moments My and M₂ act on a cut plane facing in the positive x direction.
24KN/m 12KN/m Зт A simply supported beam is loaded as shown in the figure. Assume El is constant. Determine: a. The reaction at the roller support in kN. b. The deflection at point "B" in terms of El. The deflection at the midspan in terms of El. C.
The beam ABC is subjected to a point load at the middle of segment AB and a uniformly distributed load at the segment BC, as shown in the figure. A L 20 N B 1.5W, N/m Figure 1: Overhang beam Find the deflection at the middle of the segment AB L C Set wo = 3 N/m, L = 2 m, EI = 25000 Nm². Use the method of superposition for all parts. Hint: for x > L/2 in segment AB, the solution can be obtained from the table by replacing x by L-x.
be L.A prismatic beam fixed at both ends carries a uniformly distributed load. The ratio of bending moment at supports to bending moment at midspan is