A charged particle enters a region where it experiences a drag force proportional to its velocity, that is, F d r a g = − k v . The initial velocity of the particle is v 0 . Because of this force, the particle stops and the magnitude of its displacement is L 0 = 1 0 cm . The same experiment is repeated, this time a magnetic field B (perpendicular to the particle's velocity) is applied. The particle spirals and comes to a stop. Now the the magnitude of its displacement is L 1 = 6 cm . What would be the particle's displacement L 2 in meters if the magnetic field is reduced by a factor of 2? Note that in all three cases, the initial velocity of the particle is the same. Hint: This problem can be solved without calculus.
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Using the first piece of info, we have, m × a = − k v which can be written as, m ( d v / d x ) v = − k v which simplifies to, m ( d v / d x ) = − k . Integrating this and putting the limits(from velocity v to 0), we get, mv=kl Moving on to the real part of the question, lets analyse in x and y directions, let the velocities be v(x) and v(y). Writing the force equation gives, m ( d ( v ( x ) ) / d t ) = − ( q B ) v ( y ) − k v ( x ) , and, m ( d ( v ( y ) ) / d t ) = ( q B ) v ( x ) − k v ( y ) . Here, I have also considered the magnetic force which is q ( v × B ) . Integrating these two within the limits, we get an equation involving the x and y coordinate, v(x) and v(y). We are almost there. When it comes to a stop, then v(x)=v(y)=0, so solving the linear equation we get x, y, and thus the displacement x 2 + y 2 . The final value comes out to be of the form, d = m v / ( ( q . b ) 2 + k 2 ) 1 / 2 ) = k l / ( ( ( q b ) 2 + k 2 ) 1 / 2 ) (Using the first piece of info). Now putting the values given, we get q B = ( 4 / 3 ) k . If B is halved, then d becomes 3 / 1 3 × l which is the answer.
\(v {0}\), q, B are the velocity, charge and magnetic field. We have the equation of the charge's motion: \( m\frac{d v }{dt}=q v \land B -k v \) Then \( md v =qd r \land B -kd r \) After make an integral for two members from the initial time to the stop, we have: \( m v 0 }=q r \land B -k r \) Therefore: \( L=\frac{mv {0}}{\sqrt{q^2B^2+k^2}}\) With L is the displacement of the charge. Finally: \( L {2}=\frac{2L 0L 1}{\sqrt{L^2 03L^2 1\) Numerical application: \( L_2\)=0.083 (m)
NOTE: This solution uses a bit of calculus, I couldn't avoid it.
Let us consider the first case.
Applying Newton's Law,
F
n
e
t
=
−
k
v
Since this is a 1-Dimensional case, we drop the vector notation and focus on only the magnitudes.
m d t d v = − k v
m d x d v d t d x = − k v
m d x d v v = − k v
m ⋅ d v = − k ⋅ d x
m v o ∫ 0 d v = − k 0 ∫ L o d x
m v o = k L o
Also note that, v = v o e ( − k / m ) t
Now, for the second case,
We shall go through a logical thought process.
We can agree on the fact that the second case is the
combination
of the first case and a circular motion.
So, we shall try combining the two concepts.
∙ For the first case, the solution was, v = v o e ( − k / m ) t
∙
For a circular motion the solution is,
v
x
=
v
o
sin
(
w
t
)
v
y
=
v
o
cos
(
w
t
)
, where
w
=
m
B
q
So, combining the two concepts, we have the possible (also logical) solution as,
v
x
=
v
o
e
−
λ
t
sin
(
w
t
)
v
y
=
v
o
e
−
λ
t
cos
(
w
t
)
, where
λ
=
m
k
NOTE: You can check this solution by forming a differential equation for this case, and plugging in this solution.
Now, to calculate the displacement,
We calculate the
final
(
x
,
y
)
coordinates of the particle, by integrating the above two equations, just as with the first case.
x = 0 ∫ ∞ v o e − λ t sin ( w t ) d t and,
y = 0 ∫ ∞ v o e − λ t cos ( w t ) d t
We finally get,
x = v o w 2 + λ 2 w
y = v o w 2 + λ 2 λ
Thus, the displacement is,
L 1 = x 2 + y 2 = w 2 + λ 2 v o = k 2 + B 2 q 2 m v o
Since the magnetic field is halved , we have,
L 2 = k 2 + 4 B 2 q 2 m v o
Using all the boxed equations and the values given ,
L 2 = 1 3 3 ( 0 . 1 ) m ≈ 0 . 0 8 3 2 0 m
Agreed; practically arrived at da same; Just dat u hav to knw enugh calculus to solve it; especially riting the velocity time relation for 2nd case... Nevertheless Cooooool soln :)
i too solved it the same way but i m interested to know how to arrive at the solution without using calculus. If any body has done that please share you solution.
L e t t h e p a r t i c l e i n i t i a l l y t r a v e l a l o n g x − a x i s s t a r t i n g f r o m o r i g i n . A t a n y i n s t a n t , F x = − q B V y − k V x F y = q B V x − k V y T h e a b o v e e q u a t i o n s c a n b e w r i t t e n a s m d t d V x = − q B d t d y − k d t d x m d t d V y = q B d t d x − k d t d y C a n c e l l i n g o u t d t m d V x = − q B d y − k d x m d V y = q B d x − k d y L e t x a n d y b e t h e f i n a l d i s p l a c e m e n t a l o n g x a n d y a x i s r e s p e c t i v e l y . m ∫ V o 0 d V x = − q B ∫ 0 y d y − k ∫ 0 x d x m ∫ 0 0 d V y = q B ∫ 0 x d x − k ∫ 0 y d y E v a l u a t i n g t h e i n t e g r a l , w e g e t − m V o = − q B ( y ) − k ( x ) 0 = q B ( x ) − k ( y ) S o l v i n g t h e a b o v e L i n e a r e q u a t i o n s , w e g e t x = ( q B ) 2 + k 2 m V o k a n d y = ( q B ) 2 + k 2 m V o q B s = x 2 + y 2 s = ( q B ) 2 + k 2 m V o C a s e 1 : B = 0 , s = 0 . 1 m 0 . 1 = k m V o S i n c e , m a n d V o a r e a r b i t r a r y , w e m i g h t a s w e l l t a k e m = 1 k g a n d V o = 1 m / s W h i c h g i v e s u s k = 1 0 . C a s e 2 : B = B o , s = 0 . 0 6 P l u g g i n g i n t h e v a l u e s , w e g e t q B o = 3 4 0 . C a s e 3 : B = 2 B o , s = L 3 L 3 = ( 2 q B o ) 2 + k 2 1 = ( 9 4 0 0 ) + 1 0 0 1 = 0 . 0 8 3 2 m
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In the first case, when the particle moves in a straight line, by Newton's second law, the following equality holds: m d t d v = − k v → m d t d v = − k d t d s → m ∫ d v = − k ∫ d s → m v 0 = k s → k m v 0 = s = 0 . 1 0 m
When the particle moves in a magnetic field, it is under the effect of 2 forces: the drag force with magnitude k v which is opposite to the velocity and the magnetic force B q v which is perpendicular to the velocity. Drawing out the diagram of the particle with the velocity and the forces given, we can see that the net force on the particle always forms with the velocity vector an angle α = π − θ , where sin θ = s i n α = B 2 q 2 + k 2 B q .
Since the particle spirals and comes to a stop, this implies that the net force always points to the final position (otherwise it will not be drawn toward that point) (in fact, the particle's trajectory is a logarithmic spiral), which means that the acceleration always point toward the final position. This statement implies that if we draw a line (which is called the radius) from the final position to any point on the trajectory, this line always contain the net force. Hence, the angle between the radius and the velocity is equal to the angle between the net force and the velocity, which is α .
The particle is moving in a magnetic field, therefore its angular velocity is given by ω = m B q .
In the second case, the particle starts with velocity v 0 and undergoes circular motion with radius is L 1 . We have: v 0 sin θ = ω L 1 → L 1 = ω v 0 sin θ = B q m v 0 sin θ = B 2 q 2 + k 2 m v 0 = k 2 B 2 q 2 + 1 k m v 0
Since L 1 = 0 . 0 6 and k m v 0 = 0 . 1 0 , we get k B q = 3 4 .
In the third case, the magnetic force is 2 B q v . Similarly, the angle between the velocity and the net force is α ′ = π − θ ′ , where sin θ ′ = sin α ′ = B 2 q 2 + 4 k 2 B q . Also ω ′ = 2 m B q .
Similarly, v 0 sin θ ′ = ω ′ L 2 , which gives L 2 = k 2 B 2 q 2 + 4 k 2 m v 0 = 9 1 6 + 4 2 ∗ 0 . 1 0 = 0 . 0 8 3 2 ( m ) .