Example 1: solve the equation = a?u 6x²(2y – 1)given the ax2 du sin2y and u = cosy. boundary condition that at x = 0,

Q: Solve the truth value of the well-formed formula (WFF) below. If the answer is 0 chose FALSE, is the…

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Q: Solve for M, and Mg using integration in terms of w and L. MA MB B -L/2*-L/2 -

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Q: . Determine the ratio To/T,

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Q: Velocity profile inside boundary layer is given as, U Ty = sin - sin U. 2 8 Find the value of

A: Following is the given velocity profile:

Q: QIS Determine the Displacenent at node © using Stiffness method, EA is Goms tant. 8m 6m 50 KN

A: The length of the member-1=6 m, The angle of the member-1=0o, The length of the member-2=

Q: A. B Lom Sdve for

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Q: Solve the plate shown in the figure, Include fbd on solutions

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Q: 3. Note that in the following problem b(x) is a (nonzero) constant along the entire length of the…

A: ANSWER:

Q: Derive the flexibility matrix of the plane beam shown in figure with respect to the degre shown.…

A: Given data:

Q: Q3/ Determine the magnitude and the direction of the resultant force. (Use Cartesian vector…

A: The diagram of the body is shown below,

Q: Q1 Choose the right values of X which satisfy the following inequalities* a) ->2 |2r+3

A: The detailed solution is...

Q: find the value of k so that the given DE will become exact. The given Differential equation is…

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Q: Determine the resultant of the four forces shown in the Figure.

A: Resultant is given byR=Rx2+Ry2

Q: P4 + pgz = C Verify that each additive term in the Bernoulli equation has the same dimensions. What…

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Q: 3. Deflection of beam-columns Example 1: A simply supported beam-column of length L is subjected to…

A: Its a simply supoorted beam AB with length L, carrying point load Q at midspan.Since, the load is…

Q: 8.14 Apply the step-by-step method to form n-groups from the variables Q, D, h/L, p, p, and g.…

A: In designing, applied math, and physical science, the Buckingham π hypothesis is a critical…

Q: H.w.pdf > H.W Use N.R First Method to solve the following function: x3 + 2X-2 Start with X1 = 1 ...

A: NEWTON RAPHSON METHODxn+1=xn-fxf'xfx=x3+2x-2f'x=3x2+2take  x1=1considering…

Q: SOLVE AND SHOW THE COMPLETE SOLUTION

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Q: 7. The angle of twist for a shaft subjected to twisting torque can be expressed by the equa- tion:…

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Q: In the figure shown, compute the following : (a) Components of centroid -4 in. 5 in. Ti in. [2 in.…

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Q: II. Evaluate the function below using Taylor's Series of Expansion. (10) 1 f(x)=e* at about x – a.

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Q: Solve for TA, aA, aB, and aC

A: Free body diagram (FBD): - It is a diagram in which one can see all the forces acting on an object…

Q: Find y. c, I, A,y.b the value OF

A: Find centroid:y=∑ Ay∑ A=0.02×0.0040.02+0.0042+0.02×0.120.0220.02×0.004+0.02×0.12y=0.0063137mm

Q: The function Y = cx + 4 of which "a" is a parameter is a solution to y = O True O False 业 业中

A: Given function y=Cx+(a/C)

Q: In the figure shown, compute the following : (a) Components of centroid 4 in.- 5 in. (b) Moment of…

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Q: S2) The distributed load, which is given as function of q (x) = qo (2x/34)°, acts on the ABC beam…

A: Consider the following diagram:

Q: 2 3 1 If A = -1 2 4 057 What is the cofactor of the second row, third column element? A. B. C. 3 1 5…

A: In this question a matrix is given and we are asked to find out cofactor of second row and third…

Q: Solve for the axial displacement and stress in the tapered bar shown in Figure P3-12 using one and…

A: Ao = 2 in2 L = 20 in E = 10×106 psi P = 1000 lb

Q: am given in the figure, he equation of elastic curve by integration method. (T), (M.) diagrams of…

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Q: Velocity profile inside boundary layer is given as, U sin 2 8 Find the value of

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Q: Using Galerkin's method, derive the stiffness matrix for the following beam element, which has an…

A: Given: Vx=a1x5+a2x4+a3x3+a2x2+ax+a6 The shape functions are N1, N2, and N3.

Q: Eliminate the arbitrary constant from the equation below. (x – a)^2 + y^2 = a^2 (a – constant)

A: Given data: x-a2+y2=a2       a is constant

Q: Determine the Poisson's ratio v.

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Q: Find the derivative of the equation 2x-xy-3x+2y=0

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Q: dy 2. dx solve for the general solution when y=3 and x-4 y Evect ouetions

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Q: Nétwork Diagram From the following following:

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Q: olve the unknowns and solve for the length of CA

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Q: Solve for M, and Mg using integration in terms of w and L. MA MB A L

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Q: Derive the stiffness matrix and Derive the kinema tic eyuetien

A: To perform out a precise investigation an structural engineer should decide data, for example,…

Q: [1] For the quadrilateral element shown in Figure below, evaluate the stiffness matrix coefficient…

A: Using the Gaussian Quadrature for the estimation of stiffness matrix: Using the four point rule:…

Q: A built-up section is shown in figure (a) Determine the thickness "t" of i the horizontal plate if…

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Q: Using the equation sinx – x3 +1 , determine f(3.1) utilzing Forward-difference, backward-difference,…

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Q: d) Derive an equation for structure factor, S,using Fourier analysis.

A: Structure factor describes how a material scatters incident radiation. It is required to derive…

Q: Solve for M, and Mg using integration in terms of w and L. MB MA A L –

A: In the above figure MA and MB are fixed end moments of a fixed beam loaded with uvl varying from 0-W…

Q: Velocity profile inside boundary layer is given as, U = sin Uz 2 8 Find the value of

A: We know,

Q: Using Simpson's rule Evaluate the integral of x2 - 4 if the lower limit is 0 and upper limit is 5.…

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Q: determine the value of W

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Q: 1- Use Euler's method to numerically integrate. dy -2x³ + 12²- 20x + 8.5 dx from x=0 0 to x = 4 with…

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Q: 7.2-16 Solve the preceding problem for the element shown in the figure. 24.3 MPa 62.5 MPa 0= 55°…

A: Given: Consider the figure, The normal stresses are, The shear stress is, The inclined area is…

Q: Apply Euler's method approximate the solution of the initial value theorem problem: and Runge-Kutta…

A: dydx=41+x2 y(0)= 0 h=0.2 Interval is [0,1] Euler Formula:- yn+1 = yn + h f(xn , yn)

Design of structures using FEA

An arrangement, in which various members are interconnected with their constrained relative motion, the whole arrangement is then known as a structure. The degree of freedom of such a structure is zero. In such a structure, the load can act throughout the length of the structure or at the joints.