Title: CHAPTER 3 HigherOrder Differential Equations
1CHAPTER 3Higher-Order Differential Equations
2Contents
- 3.1 Preliminary Theory Linear Equations
- 3.2 Reduction of Order
- 3.3 Homogeneous Linear Equations with Constants
Coefficients - 3.4 Undetermined Coefficients
- 3.5 Variation of Parameters
- 3.6 Cauchy-Euler Equations
- 3.7 Nonlinear Equations
- 3.8 Linear Models Initial-Value Problems
- 3.9 Linear Models Boundary-Value Problems
- 3.10 Nonlinear Models
- 3.11 Solving Models of Linear Equations
33.1 Preliminary Theory Linear Equation
- Initial-value Problem An nth-order initial
problem isSolve Subject to (
1)with n initial conditions.
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5Example 1
- The problem possesses the trivial solution y
0. Since this DE with constant coefficients,
from Theorem 3.1, hence y 0 is the only one
solution on any interval containing x 1.
6Example 2
- Please verify y 3e2x e2x 3x, is a solution
of This DE is linear and the coefficients and
g(x) are all continuous, and a2(x) ? 0 on any I
containing x 0. This DE has an unique solution
on I.
7Boundary-Value Problem
- SolveSubject to is called a boundary-value
problem (BVP).See Fig. 3.1.
8Example 3
- In example 4 of Sec. 1.1, we see the solution
of is x c1 cos 4t c2 sin 4t (2) - (a) Suppose x(0) 0, then c1 0, x(t) c2 sin
4t Furthermore, x(?/2) 0, we obtain 0 0,
hence (3)has infinite many solutions.
See Fig. 3.2. - (b) If (4)we have c1 0, c2 0, x 0
is the only solution.
9Example 3 (2)
- (c) If (5)we have c1 0, and 1 0
(contradiction).Hence (5) has no solutions.
10Fig. 3.2
11- The following DE (6)is said to be
homogeneous (7)with g(x) not
identically zero, is nonhomogeneous.
12Differential Operators
- Let dy/dx Dy. This symbol D is called a
differential operator. We define an nth-order
differential operator as (8)In
addition, we have (9)so the
differential operator L is a linear operator. - Differential Equations We can simply write the
DEs as L(y) 0 and L(y) g(x)
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15Example 4
- The function y1 x2, y2 x2 ln x are both
solutions of Then y x2 x2 ln x is also a
solution on (0, ?).
16- In other words, if the set is linearly
independent, when c1f1(x) c2f2(x) cn
fn(x) 0then c1 c2 cn 0 - Referring to Fig. 3.3, neither function is a
constant multiple of the other, then these two
functions are linearly independent.
17Example 5
- The functions f1 cos2 x, f2 sin2 x, f3
sec2 x, f4 tan2 x are linearly dependent on
the interval (-?/2, ?/2) sincec1 cos2 x c2
sin2 x c3 sec2 x c4 tan2 x 0when c1 c2
1, c3 -1, c4 1.
18Example 6
- The functions f1 x½ 5, f2 x½ 5x, f3
x 1,f4 x2 are linearly dependent on the
interval (0, ?), since f2 1? f1 5? f3 0?
f4
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22Example 7
- The functions y1 e3x, y2 e-3x are solutions
of y? 9y 0 on (-?, ?)Now for every x.
So y c1e3x c2e-3x is the general solution.
23Example 8
- The functions y 4 sinh 3x - 5e3x is a solution
of example 7 (Verify it). Observer 4
sinh 3x 5e-3x
24Example 9
- The functions y1 ex, y2 e2x , y3 e3x are
solutions of y?? 6y? 11y? 6y 0 on (-?,
?). Since for every real value of x. So y
c1ex c2 e2x c3e3x is the general solution
on (-?, ?).
25THEOREM 3.6
- Complementary Function y c1y1 c2y2 cnyn
yp yc yp complementary particular
26Example 10
- The function yp -(11/12) ½ x is a particular
solution of (11)From previous
discussions, the general solution of (11) is
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28Example 11
- We find yp1 -4x2 is a particular solution
of yp2 e2x is a particular solution of
yp3 xex is a particular solution of - From Theorem 3.7, is a solution of
29Note
- If ypi is a particular solution of (12), then
is also a particular solution of (14) when
the right-hand member is
303.2 Reduction of Order
- IntroductionWe know the general solution of
(1)is y c1y1 c2y2. Suppose y1(x)
denotes a known solution of (1). We assume the
other solution y2 has the form y2 uy1.Our goal
is to find a u(x) and this method is called
reduction of order.
31Example 1
- Given y1 ex is a solution of y? y 0, find a
second solution y2 by the method of reduction of
order. - SolutionIf y u(x) y1(x) u(x) ex, then And
Since ex ? 0, we let w u?, then
32Example 1 (2)
- Thus (2)Choosing c1 0, c2 -2, we
have y2 e-x. Because W(ex, e-x) ? 0 for every
x, they are independent.
33General Case
- Rewrite (1) as the standard form (3)Let
y1(x) denotes a known solution of (3) and y1(x) ?
0 for every x in the interval. - If we define y uy1, then we have
34- This implies that or (4)where we
let w u?. Solving (4), we have or
35- then Let c1 1, c2 0, we find (5)
36Example 2
- The function y1 x2 is a solution of Find
the general solution on (0, ?). - SolutionThe standard form is From (5) The
general solution is
373.3 Homogeneous Linear Equation with Constant
Coefficients
- Introduction (1)where ai are
constants, an ? 0. - Auxiliary EquationFor n 2,
(2)Try y emx, then (3)is
called an auxiliary equation.
38- From (3) the two roots are(1) b2 4ac gt 0
two distinct real numbers.(2) b2 4ac 0 two
equal real numbers.(3) b2 4ac lt 0 two
conjugate complex numbers.
39- Case 1 Distinct real rootsThe general solution
is (4) - Case 2 Repeated real roots
- and from (5) of Sec 3.2,
-
(5) - The general solution is (6)
40- Case 3 Conjugate complex rootsWe write
, a general solution is From Eulers
formula and
(7)
and
41- Since is a solution then setC1
C1 1 and C1 1, C2 -1 , we have two
solutions So, e?x cos ?x and e?x sin ?x
are a fundamental set of solutions, that is, the
general solution is (8)
42Example 1
- Solve the following DEs
- (a)
- (b)
- (c)
43Example 2
- Solve
- SolutionHence the solution of the IVP is
-
-
- See Fig. 3.4.
44Fig. 3.4
45Two Equations worth Knowing
-
- For the first equation (9)
- For the second equation
(10) - If c1 c2½ and c1 ½, c2 -½ in (10)
- Then, an alternative form for the general
solution is (11)
46Higher-Order Equations
- Given (12)we have (13)as
an auxiliary equation.
47Example 3
48Example 4
49Repeated complex roots
- If m1 ? i? is a complex root of multiplicity
k, then m2 ? - i? is also a complex root of
multiplicity k. The 2k linearly independent
solutions
503.4 Undetermined Coefficients
- IntroductionIf we want to solve (1)we
have to find y yc yp. Thus we introduce the
method of undetermined coefficients.
51Example 1
- Solve
- Solution We can get yc as described in Sec 3.3.
-
- Now, we want to find yp.
52Example 1 (2)
- Since the right side of the DE is a polynomial,
we set - After substitution, 2A 8Ax 4B 2Ax2 2Bx
2C 2x2 3x 6 - Then
53Example 2
- Find a particular solution of
- Solution Let yp A cos 3x B sin 3xAfter
substitution, - Then
54Example 3
- Solve (3)
- Solution We can find Let After
substitution, - Then
55Example 4
- Find yp of
- Solution First let yp AexAfter substitution,
0 8ex, (wrong guess) - Let yp AxexAfter substitution, -3Aex 8ex
Then A -8/3, yp (-8/3)xex
56Rule of Case 1
- No function in the assumed yp is part of ycTable
3.1 Trial particular solutions.
57Example 5
- Find the form of yp of (a)
- Solution We have and try There is
no duplication between yp and yc . - (b) y? 4y x cos x
- Solution We try There is also no duplication
between yp and yc .
58Example 6
- Find the form of yp of
- Solution For 3x2 For -5 sin 2x For
7xe6x - No term in duplicates a term in yc
59Rule of Case 2
- If any term in yp duplicates a term in yc, it
should be multiplied by xn, where n is the
smallest positive integer that eliminates that
duplication.
60Example 8
- Solve
- Solution First trial yp Ax B C cos x
E sin x (5)However, duplication occurs. Then
we try yp Ax B Cx cos x Ex sin x After
substitution and simplification, A 4, B 0, C
-5, E 0Then y c1 cos x c2 sin x 4x
5x cos xUsing y(?) 0, y?(?) 2, we have y
9? cos x 7 sin x 4x 5x cos x
61Example 9
- Solve
- Solution yc c1e3x c2xe3x After
substitution and simplification, A 2/3, B
8/9, C 2/3, E -6 - Then
62Example 10
- Solve
- Solution m3 m2 0, m 0, 0, -1 yc c1
c2x c3e-x yp Aex cos x Bex sin xAfter
substitution and simplification, A -1/10, B
1/5 - Then
63Example 11
- Find the form of yp of
- Solution yc c1 c2x c3x2 c4e-x Normal
trial Multiply A by x3 and (Bx2e-x Cxe-x
Ee-x) by xThen yp Ax3 Bx3e-x Cx2e-x
Exe-x
643.5 Variation of Parameters
- Some Assumptions For the DE (1)we put
(1) in the form (2)where P, Q, f are
continuous on I.
65Method of Variation of Parameters
- We try (3) After we obtain y?p,
y?p we put them into (2), then
66- Making further assumptions y1u?1 y2u? 2 0,
then from (4), y? 1u? 1 y? 2u? 2
f(x)Express the above in terms of determinants - and (5)where (6)
67Example 1
- Solve
- Solution m2 4m 4 0, m 2, 2 y1 e2x,
y2 xe2x, - Since f(x) (x 1)e2x, then
68Example 1 (2)
- From (5), Then u1 (-1/3)x3 ½ x2, u2
½ x2 xAnd
69Example 2
- Solve
- Solution y? 9y (1/4) csc 3x m2 9 0, m
3i, -3i y1 cos 3x, y2 sin 3x, f (1/4)
csc 3x - Since
70Example 2 (2)
71Example 3
- Solve
- Solution m2 1 0, m 1, -1 y1 ex, y2
e-x, f 1/x, and W(ex, e-x) -2 ThenThe
low and up bounds of the integral are x0 and x,
respectively.
72Example 3 (2)
73Higher-Order Equations
- For the DEs of the form (8)then yp
u1y1 u2y2 unyn, where yi , i 1, 2, ,
n, are the elements of yc. Thus we
have (9)and u?k Wk/W, k 1,
2, , n.
74 753.6 Cauchy-Euler Equation
- Form of Cauchy-Euler Equation
- Method of SolutionWe try y xm, since
76An Auxiliary Equation
- For n 2, y xm, then am(m 1) bm c 0,
or am2 (b a)m c 0 (1) - Case 1 Distinct Real Roots (2)
77Example 1
- Solve
- SolutionWe have a 1, b -2 , c -4 m2 3m
4 0, m -1, 4 - y c1x-1 c2x4
78Case 2 Repeated Real Roots
- Using (5) of Sec 3.2,
- Then (3)
79Example 2
- Solve
- SolutionWe have a 4, b 8, c 1 4m2 4m
1 0, m -½ , -½
80Case 3 Conjugate Complex Roots
- Higher-Order multiplicity
- Case 3 Conjugate Complex Roots m1 ? i?, m2
? i?, y C1x(? i?) C2x(? - i?)
Since xi? (eln x)i? ei? ln x cos(? ln x)
i sin(? ln x) x-i? cos (? ln x) i sin (?
ln x) -
81- For C1 C2 1, y1 x?(x i? x - i? ) 2
x?cos(? ln x) - For C1 1, C2 -1, y2 x?(x i? -x - i? )
2ix?sin(? ln x) - Since W(x?cos(? ln x), x?sin(? ln x) ) ? x2?-1
? 0 - Then y c1x? cos(? ln x) c2x? sin(? ln x)
x? c1 cos(? ln x) c2 sin(? ln x) (4)
82Example 3
- Solve
- SolutionWe have a 4, b 0 , c 17 4m2 - 4m
17 0, m ½ 2i Apply y(1) -1, y?(1)
-1/2, then c1 -1, c2 0See Fig. 3.15.
83Fig. 3.15
84Example 4
- Solve
- SolutionLet y xm, Then we have xm(m
2)(m2 4) 0 m -2, m 2i, m -2i y
c1x-2 c2 cos(2 ln x) c3 sin(2 ln x)
85Example 5
- Solve
- SolutionWe have (m 1)(m 3) 0, m 1, 3
yc c1x c2x3 , use variation of parameters,
yp u1y1 u2y2, where y1 x, y2 x3
Rewrite the DE asThen P -3/x, Q 3/x2, f
2x2ex
86Example 5 (2)
87Example 5 (3)
883.7 Nonlinear Equations
- Example 1 Solve
- SolutionThis nonlinear equation misses y term.
Let u(x) y?, then du/dx y?, or
(This form is just for convenience)Since u-1
1/y?,So,
89Example 2
- Solve
- SolutionThis nonlinear equation misses x term.
Let u(x) y?, then y? du/dx
(du/dy)(dy/dx) u du/dy or lnu
lny c1, u c2y (where )Since
u dy/dx c2y, dy/y c2 dx lny c2x
c3,
90Example 3
- Assume (1)exists. If we further assume
y(x) possesses a Taylor series centered at
0 (2)Remember that y(0) -1, y?(0)
1. From the original DE, y?(0) 0 y(0) y(0)2
-2. Then (3)
91Example 3 (2)
- (4) (5)and so on. So we can
use the same method to obtain y(3)(0) 4,
y(4)(0) -8, Then
923.8 Linear Models IVP
- Newtons LawSee Fig. 3.18, we have
(1)
Fig. 3.19
Fig. 3.18
93Free Undamped Motion
- From (1), we have (2)where ? k/m. (2)
is called a simple harmonic motion, or free
undamped motion. - From (2), the general solution is
(3)Period T 2?/?, frequency f 1/T ?/2?.
94Example 1
- A mass weighing 2 pounds stretches a spring 6
inches. At t 0, the mass is released from a 8
inches below the equilibrium position with an
upward velocity 4/3 ft/s. Determine the equation
of motion. - SolutionUnit convert 6 in 1/2 ft 8 in
2/3 ft, m W/g 1/16 slugFrom Hookes Law,
2 k(1/2), k 4 lb/ft Hence (1) gives
95Example 1 (2)
- together with x(0) 2/3, x?(0) -4/3.Since ?2
k/m 64, ? 8, the solution is x(t) c1
cos 8t c2 sin 8t (4)Applying the initial
condition, we have (5)
96Alternate form of x(t)
- (3) can be written as x(t) A sin(?t ?)
(6)where and ? is a phase angle,
(7) (8)
(9)
97Fig. 3.20
98Example 2
- Solution (5) is x(t) (2/3) cos 8t - (1/6) sin
8t A sin(?t ?)Then However it is not
the solution, since we know tan-1 (/-) will
locate in the second quadrantThen
so (9)The period is T 2?/8 ?/4.
99Fig. 3.21
- Fig. 3.21 shows the motion.
100Free Damped Motion
- If the DE is as (10)where ? is a
positive damping constant. Then x?(t) (?/m)x?
(k/m)x 0 can be written as (11)where
2? ?/m, ?2 k/m (12)The auxiliary
equation is m2 2?m ?2 0, and the roots are
101Case 1
- ?2 ?2 gt 0, then (13)It is said to
be overdamped. See Fig. 3.23.
Fig. 3.23
102Case 2
- ?2 ?2 0. then
(14) - It is said to be critically damped. See Fig.
3.24.
Fig. 3.24
103Case 3
- ?2 ?2 lt 0, then (15)It is said
to be underdamped. See Fig. 3.25.
104Fig. 3.25
105Example 3
- The solution of is (16)See Fig.
3.26.
106Fig. 3.26
107Example 4
- A mass weighing 8 pounds stretches a spring 2
feet. Assuming a damping force equal to 2 times
the instantaneous velocity exists. At t 0, the
mass is released from the equilibrium position
with an upward velocity 3 ft/s. Determine the
equation of motion. - SolutionFrom Hookes Law, 8 k (2), k 4
lb/ft, and m W/g 8/32 ¼ slug, hence
(17)
108Example 4 (2)
- m2 8m 16 0, m -4, -4 x(t) c1 e-4t
c2t e-4t (18)Initial conditions x(0) 0,
x?(0) -3, then x(t) -3t e-4t (19)See
Fig. 3.27.
109Fig. 3.27
110Example 5
- A mass weighing 16 pounds stretches a spring from
5 feet to 8.2 feet. t. Assuming a damping force
is equal to the instantaneous velocity exists. At
t 0, the mass is released from rest at a point
2 feet above the equilibrium position. Determine
the equation of motion. - SolutionFrom Hookes Law, 16 k (3.2), k 5
lb/ft, and m W/g 16/32 ½ slug, hence
(20) m2 2m 10 0, m -1 3i,
-1 - 3i
111Example 5 (2)
- (21)Initial conditions x(0) -2,
x?(0) 0, then (22)
112Alternate form of x(t)
- (22) can be written as (23)where
and - Thus
113DE of Driven Motion with Damping
- As in Fig. 3.28, (24) (25)wh
ere
114Fig. 3.28
115Example 6
- Interpret and solve (26)
- SolutionInterpret m 1/5, k 2, ? 1.2,
f(t) 5 cos 4t release from rest at a point ½
below Sol
116Example 6 (2)
- Assuming xp(t) A cos 4t B sin 4t,we have A
-25/102, B 50/51, then Using x(0) 1/2,
x?(0) 0 c1 38/51, c2 -86/51,
(28)
117Transient and Steady-State
- Graph of (28) is shown in Fig. 3.29.
- xc(t) will vanish at t ? ? transient termxp(t)
will still remain at t ? ? steady-state
term
Fig. 3.29
118Example 7
- The solution of isSee Fig. 3.30.
119Fig. 3.30
120Example 8
- Solve where F0 is a constant and ? ? ?.
- Solution xc c1 cos ?t c2 sin ?t Let xp
A cos ?t B sin ?t, after substitution, A
0, B F0/(?2-? 2),
121Example 8 (2)
- Since x(0) 0, x?(0) 0, then
- Thus (30)
122Pure Resonance
- When ? ?, we consider the case ? ? ?.
(31)
123Fig. 3.31
- When t ? ?, the displacements become large.In
fact, x(tn) ? ? when tn n?/?, n 1, 2,
..As shown in Fig. 3.31, it is said to be pure
resonance.
124LRC-Series Circuits
- The following equation is the DE of forced motion
with damping (32)If i(t) denotes the
current shown in Fig. 3.32, then
(33)Since i dq/dt, we
have (34)
125Fig. 3.32
- Overdampered if R2-4L/C gt 0
- Critically dampered if R2-4L/C 0
- Underdampered if R2-4L/C gt 0
126Example 9
- Find q(t) in Fig. 3.32, where L 0.25 henry, R
10 ohms, C 0.001 farad, E(t) 0, q(0) q0
coulombs, and i(0) 0 ampere. - SolutionUsing the given dataAs described
before, Using q(0) q0, i(0) q?(0) 0, c1
q0, c2 q0/3
127Example 10
- Find the steady-state qp(t) and the steady-state
current in an LRC-series circuit when E(t) E0
sin ?t . - SolutionLet qp(t) A sin ?t B cos ?t,
128Example 10 (2)
- If
- If
- Using the similar method, we haveSo
- Note X and Z are called the reactance and
impedance, respectively.
1293.9 Linear Models BVP
- Deflection of a BeamThe bending moment M(x) at
a point x along the beam is related to the load
per unit length w(x) by (1)In addition,
M(x) is proportional to the curvature ? of the
elastic curve M(x) EI? (2)where E, I
are constants.
130- From calculus, we have ? ? y?, when the
deflection y(x) is small. Finally we
have (3)Then (4)
131Terminology
132Example 1
- A beam of length L is embedded at both ends. Find
the deflection of the beam if a constant load w0
is uniformly distributed along its length, that
is, w(x) w0 , 0 lt x lt L - SolutionFrom (4) we have Embedded ends
means We have m4 0, yc(x) c1 c2x c3x2
c4x3, and
133Example 1 (2)
- So Using the boundary conditions, we have c1
0, c2 0, c3 w0L2/24EI, c4
-w0L/12EIChoosing w0 24EI and L 1, we
have Fig. 3.42.
134Fig. 3.42
135Example 2
- Solve
- SolutionCase 1 ? 0 y c1x c2, y(0)
c2 0, y(L) c1L 0, c1 0then y 0,
trivial solution. - Case 2 ? lt 0, ? -?2, ? gt 0Choose y c1 cosh
?x c2 sinh ?x y(0) 0, c1 0 y(L) 0, c2
0 then y 0, trivial solution.
136Example 2 (2)
- Case 3 ? gt 0, ? ?2, ? gt 0Choose y c1 cos
?x c2 sin ?x y(0) 0, c1 0 y(L) 0, c2
sin ?L 0 If c2 0, y 0, trivial
solution.So c2 ? 0, sin ?L 0, ?L n?, ?
n?/L Thus, y c2 sin (n?x/L) is a solution
for each n.
137Example 2 (3)
- Simply take c2 1, for each the
corresponding function - Note ?n (n?/L)2, n 1, 2, 3, are known as
characteristic values or eigenvalues. yn sin
(n?x/L) are called characteristic functions or
eigenfunctions.
138Bulking of a Thin Vertical Column
- Referring to Fig. 3.43, the DE is
-
(5)where P is a constant vertical compressive
force applied to the columns top.
Fig. 3.43
139Example 3
- Referring to Fig. 3.43, when the column is hinged
at both ends, find the deflection. - SolutionThe boundary-value problem is From
the intuitive view, if the load P is not great
enough, there is no deflection. The question is
For what values of P does the given BVP possess
nontrivial solutions?
140Example 3 (2)
- By writing ? P/EI, we see is identical to
example 2. From Case 3, the deflection curves are
yn c2 sin (n?x/L), corresponding to eigenvalues
?n Pn/EI n2?2/L2, n 1, 2, 3, - Physically, only Pn EIn2?2/L2, deflection
occurs.We call these Pn the critical loads and
the smallest P P1 EI?2/L2 is called the Euler
load, andy1 c2 sin(?x/L) is known as the first
buckling mode.See Fig. 3.44
141Fig. 3.44
142Rotating String
- The simple DEy? ?y 0 (6)occurs again as a
model of a rotating string. See Fig. 3.45.
Fig 3.45
143- We have the net vertical force F T sin ?2 T
sin ?1 (7)When ?1 and ?2 are small, sin ?2
? tan ?2 , sin ?1 ? tan ?1Since tan?2, tan?1 are
slopes of the lines containing the vectors T1 and
T2, then tan ?2 y?(x ?x), tan ?1
y?(x)Thus (7) becomes (8)Because F
ma, m ??x, centripetal acceleration a r?2.
With ?x small, we take r y.
144- Thus (9)Letting (8) (9), we
have (10)For ?x close to zero, we
have (11)And the boundary conditions
are y(0) y(L) 0.
1453.10 Nonlinear Models
- Nonlinerar SpringsThe model (1)when
F(x) kx is said to be a linear spring.
However, (2)is a nonlinear spring.
Another model of a free/mass system with
damping -
(3)
146Hard and Soft Springs
- F(x) kx k1x3 is said to be hard if k1 gt
0and is soft, if k1 lt 0. See Fig. 3.50.
Fig. 3.50
147Example 1
- The DEs (4)and (5)are special
cases of (2). Fig. 3.51 shows the graph from a
numerical solver.
148Fig. 3.51
149Nonlinear Pendulum
- The model of a simple pendulum is shown in Fig.
3.52. From the figure, the arc s of a circle of
radius l is related to the center ? by s l?.
Angle acceleration is a s? l??, the force
Then (6)
Fig. 3.52
150Linearization
- Since If we use only the first two terms,
If ? is small, (7)
151Example 2
- Fig. 3.53 shows some results with different
initial conditions by a solver. We can see if the
initial velocity is great enough, it will go out
of bounds.
Fig. 3.53
152Telephone Wire
- Recalling from (17) in Sec. 1.3 and Fig. 1.26
dy/dx W/T1, it can be modified
as (8)where ? is the density and s is
the arc length.Since the length s is
(9)
153- then (10)Differentiating (8) w.s.t
x and using (10), then (11)
154Example 3
- From Fig. 1.26, we obtain y(0) a, y ?(0) 0.
Let u y?, equation (11) becomesThus Now
y?(0) u(0) 0, sinh-10 0 c1 Since u
sinh(?x/T1) dy/dx, then Using y(0) a, c2
a - (T1/?)
155Rocket Motion
- From Fig 3.54, we have
- (12)
- when y R, kMm/R2 Mg, k gR2/M, then
(13)
Fig. 3.54
156Variable Mass
- Assuming the mass is variable, then F ma should
be modified as (14)
157Example 4
- A uniform 10-foot-long chain is coiled loosely on
the ground. On end is pulled vertically by a
force of 5 lb. The chain weigh 1 lb per foot.
Determine the height of the end at time t. - SolutionLet x(t) the height v(t) dx/dt
(velocity) W x?1 x (weight) m W/g
x/32 (mass) F 5 W (net force)
158Example 4 (2)
- Then (15)Since v dx/dt (16)
is of the form F(x, x?, x?) 0Since v x?,
andthen (15) becomes (17)
159Example 4 (3)
- Rewriting (17) as (v232x 160) dx xv dv
0 (18)(18) can be multiplied by an integrating
factor to become exact, where we can find the
integrating factor is ?(x) x. ThenUse the
method in Sec. 2.4 (19)Since x(0) 0,
then c1 0. By solving (19) 0, for v dx/dt
gt 0, we get
160Example 4 (4)
- Thus (20)Using x(0) 0 again,
, we square both sides of (20)
and solve for x (21)
1613.11 Solving Systems of Linear Equations
- Coupled Spring/Mass SystemFrom Fig. 3.58 and
Newtons Law - (1)
Fig. 3.58
162Method of Solution
- Consider dx/dt 3y, dy/dt 2x or Dx 3y
0, 2x Dy 0 (2)Then, multiplying the
first by D, the second by -3, and then
eliminating y, gives D2x 6x 0 (3)Sim
ilar method can give (4)
163- Return to the original equations, dx/dt
3yafter substituting and simplification, we
have (5)
164Example 1
- Solve Dx (D 2)y 0 (D 3)x
2y 0 (6) - SolutionMultiplying the first by D 3, the
second by D, then subtracting, (D 3)(D 2)
2Dy 0 (D2 D 6)y 0then y(t) c1e2t
c2e-3t (7)
165Example 1 (2)
- Using the similar method, x(t) c3e2t
c4e-3t (8)Substituting (7) and (8) into the
first equation of (6), (4c1 2c3)e2t (-c2
3c4)e-3t 0Then 4c1 2c3 0 -c2 3c4 c3
2c1, c4 ?c2
166Example 2
- Solve x? 4x y? t2 x? x y? 0 (9)
- Solution (D 4)x D2y t2 (D 1)x Dy
0 (10)By eliminating x, then
and m 0, 2i, -2iLet
then we can get A 1/12, B ¼ ,
C -1/8.
167Example 2 (2)
- Thus (11)Similar method to get
x(t) Then m 2i, -2i, Let xp(t) At2 Bt
C, thenwe can get A -1/4, B 0, C 1/8
168Example 2 (3)
- Thus (12)By using the second equation
of (9), we have
169Example 4
- Solve (13) with
- Solution Then
170Example 4 (2)
- Using the same method, we have (14)
171Fig. 3.59
172Thank You for Your Attention