Classical Mechanics
Classical Mechanics
5th Edition
ISBN: 9781891389221
Author: John R. Taylor
Publisher: University Science Books
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Chapter 6, Problem 6.23P

(a)

To determine

The plane’s ground speed and plane’s position.

(a)

Expert Solution
Check Mark

Answer to Problem 6.23P

The total plane’s ground speed in terms of V, v0 and ϕ is, (v0cosϕ+Vy)2+(v0sinϕ)2

Explanation of Solution

Write the expression for the speed of the wind along east direction is,

  vmind=Vyx^        (I)

Here, x and y are measured in east and north respectively.

Let v0 be the speed of the aircraft. From the figure, the total horizontal component of the speed of the aircraft-wind system is,

  vx=v0cosϕ+Vy        (II)

Similarly the vertical component of the speed of the aircraft is

  vy=v0sinϕ        (III)

Conclusion:

Thus, the expression for the total plane’s ground speed is,

  v=vx2+vy2        (IV)

Substitute expression (I) and (II) in equation (IV),

  v=(v0cosϕ+Vy)2+(v0sinϕ)2

Hence the total plane’s ground speed in terms of V, v0 and ϕ is, (v0cosϕ+Vy)2+(v0sinϕ)2

(b)

To determine

The time of flight as an integral of the form 0Dfdx

(b)

Expert Solution
Check Mark

Answer to Problem 6.23P

The required expression for the integrand f is (1+12y2)v0(1+ky)

Explanation of Solution

Write the expr4ession for the plane’s ground speed,

  v=(v0cosϕ+Vy)2+(v0sinϕ)2=(v02cos2ϕ+V2y2+2v0Vycosϕ)+(v0sinϕ)2=v02(cos2ϕ+sin2ϕ)+V2y2+2v0Vycosϕ=v02+V2y2+2v0Vycosϕ        (I)

Assume that the angel ϕ is very small. From the properties of the cosine function, the cosine function is equal to one for small angles, that is cosϕ=1 Thus, the plane’s ground speed equation becomes as,

  v=v02+2v0Vy+V2y2=(v0+Vy)2=v0+Vy        (II)

Conclusion:

The expression for the given path from the town O (origin) to town P is y=y(x). Thus the expression for the distance traveled by the plane is,

  ds=dx2+dy2        (III)

The differential form of the variable     y as a function of x can be written as,

  y=dydx        (IV)

Substitute expression (IV) in expression (III)

  ds=dx2+(ydx)2=dx2+(ydx)2=(1+y2)dx2=1+ydx

The expression for the time taken by the plane to cover the distance from the point O to point P is,

  t=OPdsv

Let D be the distance covered by the plane due east. Thus, the time of flight is,

    t=ODdsv

Substitute 1+y2dx for ds and vo+Vy for V

  t=OD1+y2dxvo+Vy=OD(1+12y2)dxvo+Vy=OD(1+12y2)dxvo(1+Vyv0)

Let Vv0=k the time of flight equation becomes as,

  t=OD(1+12y2)dxvo(1+ky)

Compare this equation with standard form of Euler-Lagrange equation

S=x1x2f(y(x),y(x),x)dx and the variables x and y are interchanged.

  f(y,y,x)=(1+12y2)v0(1+ky)

Therefore the required expression for the integrand f is (1+12y2)v0(1+ky)

(c)

To determine

The distance and the time by the plane along in its path

(c)

Expert Solution
Check Mark

Answer to Problem 6.23P

The distance traveled by the plane due north is 366miles and the time saved by the plane along in its path is 27min.

Explanation of Solution

Write the Euler-Lagrange equation for all the values of x ,

  fyddxfy=0        (I)

Determine the value of fy,

  fy=y((1+12y2)v0(1+ky))=1v0(1+12y2)y(11+ky)=1v0(1+12y2)k(1+ky)2

Similarly, determine the values of fy

  fy=y((1+12y2)v0(1+ky))=1v0(1+ky)y(1+12y2)=1v0(1+ky)(0+12(2)y)=yv0(1+ky)        (II)

Calculate the value of ddxfy

   ddxfy=ddx(yv0(1+ky))=1v0ddx(y(1+ky))=1v0(y(1+ky)1+y(1)(ky)(1+ky)2)=1v0(y(1+ky)1+(ky2)(1+ky)2)        (III)

Conclusion:

Thus, the Euler-Lagrange equation becomes as,

  1v0(1+12y2)k(1+ky)21v0(y(1+ky)1+(ky2)(1+ky)2)=0(1+12y2)k(1+ky)2(y(1+ky)1+(ky2)(1+ky)2)=01(1+ky)((1+12y2)k(1+ky)+yky2(1+ky))=0(1+12y2)k(1+ky)+yky2(1+ky)=0y(1+ky)ky+(k/2)y2+k(1+ky)=0y(1+ky)(k/2)y2+k=0        (IV)

The path of the plane is defined as,

  y(x)=λx(Dx)=λxDλx2

Differentiate the equation on both sides with respect to x

  y=λD2λx

Similarly, differentiate the equation y=λD2λx on both sides with respect to x.

  y=2λ

Substitute λxDλx2 for y, λD2λx for y and 2λ for y in the equation (IV),

  y(1+ky)(k/2)y2+k=0(2y)(1+k(λxDλx2)12k(λD2λx)2+k)=02λ2λ2xDk+2λ2x2k12kλ2D212k4λ2x2+12k(2(λD)(dλk))+k=02λ2kλ2xD+2kλ2x212kλ2x22kλ2x2+2kλ2xD+k=02λ12kλ2D2+k=0

The equation can be written as in the form of quadratic equation,

  2λ12kλ2D2+k=04λkλ2D2+2k=0(kD2)λ24λ+2k=0λ2+(4kD2)λ(2D2)=0

The roots of the quadratic equation λ2+(4kD2)λ(2D2)=0 are.

  λ=(4kD2)±(4kD2)24(1)(2D2)2(1)λ=(4kD2)±(4(4+2k2D2)(kD2)2)2(1)λ=4±24+2k2D22kD2λ=±4+2k2D22kD2

Thus the solution λ=±4+2k2D22kD2 satisfies the Euler-Lagrange equation.

Thus the expression for the constant λ is

  λ=±4+2k2D22kD2        (V)

Substitute Vv0 for k in above expression(V)

  λ=±4+2(Vv0)2D22(Vv0)D2        (VI)

Substitute 0.5mph/mi for V , 500mph for v0 and 2000mi for D in expression (VI)

  λ=±4+2(0.5mph/mi500mph)2(2000mi)22(0.5mph/mi500mph)(2000mi)2=3.66×104

The expression for the maximum displacement of the plane due north is,

  ymax=λD24

Substitute 3.66×104 for λ and 2000mi for D

  ymax=(3.66×104)(2000mi)24=366mi

Therefore, the distance traveled by the plane due north is 366mi.

The expression for the time along the path is,

  t=OD(1+12y2)dxvo(1+ky)t=1v0OD(1+12y2)dxvo(1+ky)        (VII)

Substitute λD2λx for y, Vv0 for k and λx(Dx) for y expression,

  t=1v0OD(1+12(λD2λx)2)dx(1+(Vvo)λx(Dx))        (VIII)

Let x=Ds, then dx=Dds thus, the equation (VIII) becomes as,

  t=Dv001(1+12(λ2D2)(12s)2)ds(1+(Vvo)λD2s(1s))        (IX)

Substitute 0.5mph/mi for V , 500mph for v0 3.66×104 for λ and 2000mi for D in expression (IX)

  t=Dv001(1+12((3.66×104)2(2000mi)2)(12s)2)ds(1+(0.5mph/mi500mph)(3.66×104)(2000mi)2s(1s))t=Dv001(1+(0.268)(12s)2)ds(1+(1.464)s(1s))t=(0.889)Dv0

Substitute 500mph for v0 and 200mi for D in the equation t=(0.889)Dv0,

  t=(0.889)200mi500mph=3.556h

The time taken by the plane to travel a distance along the direct path is,

  t=Dv0

Substitute 500mph for v0 and 200mi for D in the equation t=Dv0,

  t=200mi500mph=4h

Thus, the time saved by the plane along in its path is,

  Δt=4h-3.556h=0.444h(60min1h)=26.64min

Rounding off to two significant figures, the time saved by the plane along in its path is 27min

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