Please solve using double integration method, showing all steps please Using the double-integration method:a) Determine the equations of the elastic curve (deflection) and slope of the beamshown in Figure 4. Assume the x coordinate begins at the free end (point B).b) Given E = 29,000 ksi and I = 600 in4, specify the slope and deflection at pointB.PNote: Use units of inches for lengths and kips for forces throughout your calculations.Hint: 2kft1 k15 ft = 180 in6 in'A2 klf-EI15 ft-CB58

Detailed explanation: Step 1: Define the coordinate system. Let's define the coordinate system with…

Answered: Using the double-integration method: a)…

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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A.) It is the boundary condition for fixed support Choices: Both choices Y=0 Y’=0 Either of the choices B.) It is a type of simple stress acting parallel to an area Choices: Flexural stress Shear stress Axial stress Bearing stress C.) For concentric row of bolts in a coupling connection, the shear deformations in the bolts is proportional to the: Choices Modulus of rigidity Diameter of bolt circle Radial distance Number of bolts note: please help us in the word meaing sample problems thank you
For the simply-supported and cantilever beams given below, use Singularity Functions to determine slope and displacement equations. Provide graphs of both slope and displacement versus position along the beam. A A 5 ft B * B 5 ft 5 ft 27 kips E 20 ft 45 kip-ft 11 kips 5 ft 3.5 kips/ft 20 ft C 5 ft 5 ft 2.3 kips/ft 5 ft ]c S ft D
The person who answered this previously used sin and cos-please use geometry for example 3,4,5 triangles things of that nature. Thanks
Use the graphical method to construct the shear-force and bending-moment diagrams for the beam shown. Let a=4.0 ft, b-9.0 ft. c=4.0 ft, d=3.0ft, w=8 kips/ft and P = 66 kips. Construct the shear-force and bending-moment diagrams on paper and use the results to answer the questions in the subsequent parts of this GO exercise. B B ÎÎÎÎÎÎ Answers: Ay=i b d For this loading, calculate the reaction forces Ay and Ey acting on the beam. Positive values for the reactions are indicated by the directions of the red arrows shown on the free-body diagram below. (Note: Since Ax = 0, it has been omitted from the free-body diagram.) W C b C C D E kips, Ey = i E X Ey kips.
L=9m W=5kN/m 360 UB 50.7
Beta = 2 Im in hurry please answer Just one step is enough for me please send me quickly
I’m struggling with q 6 7 8
Perform double integration of the bending moment equations. You will obtain deflections in this form (can be found in the image attached) Calculate: the value of the constant integration C2. Enter your answer in kNm2 to three decimal places. b) the value of the integration constant C4. Enter your answer in kNm2 to three decimal places. c) the value of the deflection at point C. Enter your answer in mm to three decimal places.
let d={{.006, .002, .001},{.002, .004, .002},{.001, .002, .006}} be a flexibility matrix, with flexibility measured in inches per pound, and forces being applied at points 1, 2, and 3. Compute the stiffness matrix D^-1. List the forces needed to produce a deflection of .05in. at point 3, with zero deflections at the other points.
Problem 7: Non-circular cross section shaft related to torque problems are difficult to be solved using the basic theory as for circular shaft. Your role is to make use of FAE to analyze the stress in squared cross section shaft shown in Figure.5. g= 6.5(10%) N/cm? e = 0.035 deg 0.5 cm 0.5 cm 0.5 cm- 0.5 cm Figure.5: Squared cross section shaft applied to torque T as 3D model Provide justified explanation and recommendations to simplify the problem from three-dimensional (3D) to two- dimensional (2D). b. а. If the governing boundary value problem equation of such a problem can be given by: + 2g0 = 0, dy? $(x,y) at boundary is 0 dx2
0.0107 0.0043 0.0021 Let D= 0.0043 0.0085 0.0043 be a flexibility matrix, with flexibility measured in inches per pound. Suppose that forces of 40, 20, and 50 lb are applied to a beam at points 1, 2, and 3, respectively. Find the corresponding 0.0021 0.0043 0.0107 deflections y1. y2, and y3- #1 y1 = inch(es) (Round to the nearest thousandth as needed.)

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