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In Problems 10–13, use the vectorized Euler method with = 0.25 to find an approximation for the solution to the given initial value problem on the specified interval.

y''+ty'+y=0;y(0)=1,y'(0)=0on[0,1]

Short Answer

Expert verified

y(0.25)=1y(0.5)=0.9375y(0.75)=0.8164y(1)=0.651855

Step by step solution

01

Transform equation

Here h=0.25 0n [0,1]

The equations can be written as;

x1(t)=y(t)x2(t)=x'(t)

The transformation of the equation is;

x'1(t)=x2(t)x'2(t)=-x1-tx2

The initial conditions are;

x1(0)=y1(0)=1=x1,0x2(0)=y'(0)=0=x2,0

02

Apply Euler’s method.

Now,

xn+1=xn+hf(tn,xn)

tn+1=tn+h=0+0.25x1(0.25)=x1,1=1x2(0.25)=x2,1=-0.25

And

tn+1=tn+ht2=0.25+0.25x1(0.5)=x1,2=0.9375x2(0.5)=x2,2=-0.484375

t3=0.5+0.25=0.75x1(0.75)=x1,3=0.816406x2(0.75)=x2,3=-0.658203

t4=0.75+0.25=1x1(1)=x1,4=0.651855x2(1)=x2,4=-0.738891

This is the required result.

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Most popular questions from this chapter

For the interconnected tanks problem of Section5.1, page241, suppose that instead of pure water being fed into the tankA, a brine solution with concentration0.2kg/L is used; all other data remain the same. Determine the mass of salt in each tank at time tif the initial masses are and y0=0.3kg.

In Problems 3–6, find the critical point set for the given system.

dxdt=y2-3y+2,dydt=(x-1)(y-2)

Rigid Body Nutation. Euler’s equations describe the motion of the principal-axis components of the angular velocity of a freely rotating rigid body (such as a space station), as seen by an observer rotating with the body (the astronauts, for example). This motion is called nutation. If the angular velocity components are denoted by x, y, and z, then an example of Euler’s equations is the three-dimensional autonomous system

\(\begin{array}{l}\frac{{{\bf{dx}}}}{{{\bf{dt}}}}{\bf{ = yz}}\\\frac{{{\bf{dy}}}}{{{\bf{dt}}}}{\bf{ = - 2xz}}\\\frac{{{\bf{dz}}}}{{{\bf{dt}}}}{\bf{ = xy}}\end{array}\)

The trajectory of a solution x(t),y(t), z(t) to these equations is the curve generated by the points (x(t), y(t), z(t) ) in xyz-phase space as t varies over an interval I.

(a) Show that each trajectory of this system lies on the surface of a (possibly degenerate) sphere centered at the origin (0, 0, 0).[Hint: Compute\(\frac{{\bf{d}}}{{{\bf{dt}}}}{\bf{(}}{{\bf{x}}^{\bf{2}}}{\bf{ + }}{{\bf{y}}^{\bf{2}}}{\bf{ + }}{{\bf{z}}^{\bf{2}}}{\bf{)}}\)What does this say about the magnitude of the angular velocity vector?

(b) Find all the critical points of the system, i.e., all points\({\bf{(}}{{\bf{x}}_{\bf{o}}}{\bf{,}}{{\bf{y}}_{\bf{o}}}{\bf{,}}{{\bf{z}}_{\bf{o}}}{\bf{)}}\) such that \({\bf{x(t) = }}{{\bf{x}}_{\bf{o}}}{\bf{,y(t) = }}{{\bf{y}}_{\bf{o}}}{\bf{,z(t) = }}{{\bf{z}}_{\bf{o}}}\) is a solution. For such solutions, the angular velocity vector remains constant in the body system.

(c) Show that the trajectories of the system lie along the intersection of a sphere and an elliptic cylinder of the form\({{\bf{y}}^{\bf{2}}}{\bf{ + 2}}{{\bf{x}}^{\bf{2}}}{\bf{ = C}}\) for some constant C. [Hint: Consider the expression for dy/dx implied by Euler’s equations.]

(d) Using the results of parts (b) and (c), argue that the trajectories of this system are closed curves. What does this say about the corresponding solutions?

(e) Figure 5.19 displays some typical trajectories for this system. Discuss the stability of the three critical points indicated on the positive axes.

In Problems 3 – 18, use the elimination method to find a general solution for the given linear system, where differentiation is with respect to t.

dxdt=x-4ydydt=x+y

In Problems 3–6, find the critical point set for the given system.

dxdt=y-1dydt=x+y+5

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