2. Curved block ABC, AB = parabolic curve and BC is straight in the horizontal direction. Point B is the top of the curvature of the block with a slope of 0^o. Horizontal distance AB = 6m;BC=2m and vertical distance AB=2m. The load is evenly distributed q works from A to E; moment coupling load M and concentrated load P with slope tan = 0.75 acting at point C. The equation of curvature of parabolic beam AB is y= a+bx+cx^2. question A.Hitungof style in the N, L, M in pieces D, E and Bkanan and specify its nature(ND,LD,MD,NE,LE,ME,NB,LB,MB) B.Draw the force field diagram in bending moment (M plane) for the beam ABC q = 600 N/m' P = 1500 N Mc= 2400 Nm C= ujung bebas 2 m B = rol 2 m 2 m 2 m tan a = 0.75 3 2 m A = sendi

2. Curved block ABC, AB = parabolic curve and BC is straight in the horizontal direction. Point B is the top of the curvature of the block with a slope of 0^o. Horizontal distance AB = 6m;BC=2m and vertical distance AB=2m. The load is evenly distributed q works from A to E; moment coupling load M and concentrated load P with slope tan = 0.75 acting at point C. The equation of curvature of parabolic beam AB is y= a+bx+cx^2. question A.Hitungof style in the N, L, M in pieces D, E and Bkanan and specify its nature(ND,LD,MD,NE,LE,ME,NB,LB,MB) B.Draw the force field diagram in bending moment (M plane) for the beam ABC q = 600 N/m' P = 1500 N Mc= 2400 Nm C= ujung bebas 2 m B = rol 2 m 2 m 2 m tan a = 0.75 3 2 m A = sendi

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question 1) F=11 kN single load, M=22 kN.m moment andA distributed load of w=5 kN/m is effective. The length L is also given as L=5 m.The cross-sectional properties of the beam are; body height Hg=218 mm, body thickness xg=18 mm, flangewidth xf=190 mm, flange height yF13 mm. Point E on the section is flange-It is located just below the body junction. In the section taken from the B line of the beamIt is desired to determine the stress state. According to this;Question 1-A) Find the support response (DY) at point D. (Return your result in kNQuestion 1-B) Find the support response (Ay) at point A. (Return your result in kNwrite.)Question 1-C) Find the shear force (VB) at point B. (KN your resulttype in size.)
Plot the bending moment diagram
Question 1) F=35 kN single load, M=45 kN.m moment and w=16 kN/m distributed load are acting on the beam whose loading condition is given in the figure. The length L is also given as L=4 m. The cross-sectional properties of the beam are; body height yg=225 mm, body thickness xg=14 mm, flange width xf=194 mm, flange height yf=11 mm. Point P on the section is located just above the flange-body junction. It is desired to determine the stress state at the P point in the section taken from the B line of the beam. According to this;Question1-A) Find the shear force (VB) at point B. (Write your result in kN.)Question1-B) Find the bending moment (MB) at point B. (Write your result in kN.m.)Question 1-C) Find the moment of inertia of the beam section. (Do your operations by converting the lengths to meters. Take at least 4 digits for the decimal part of your result and use the expression E for the decimal part. Write it as 5E-3 instead of 0.005.)
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In a cantilever beam, the bending moment is maximum at its support end. Select one: True False
A uniform distributed load of 4 kN/m is applied to a cantilever beam as shown. What is the resisting bending moment equation for any section of the beam? 4 kN/m Select one: O a. M, = -2x³ kNm O b. Mr = -2x² kNm O c. M₁ = -4x² kNm O d. Mr = -8x kNm O e. None of these options Ai →X 2M
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The figure below shows two solid homogenous rectangular beam sections with (breadth x depth) dimensions in two different orientations as follows: Beam Section Orientation A (t mm x 2t mm); and Beam Section Orientation B (2t mm xt mm). Both beams sag when subjected to the same loading and support conditions resulting in compressive stresses above the centroid line (neutral axis). Which statement accurately describes the relative maximum compressive stress (ocompression) between these beam section orientations? * Maximum compressive stress (acompression) in orientation A is greater than orientation B by a factor of 4. Maximum compressive stress (acompression) in orientation B is greater than orientation A by a factor of 4. * Maximum compressive stress (acompression) in orientation B is greater than orientation A by a factor of 2. 4 Maximum compressive stress (acompression) in orientation A is greater than orientation B by a factor of 2.