A massive particle is launched from ground level with a velocity of magnitude v and a launch angle of θ with respect to the ground.
Suppose a large (essentially infinite) number of launches take place. Over the many trials, θ varies uniformly between 0 and 2 π , and v varies uniformly between 0 and v max .
If there is a uniform downward gravitational acceleration g , the expected average distance of the landing point from the launch point (assuming level ground) can be expressed as b a π g v max 2 , where a and b are coprime positive integers.
Determine a + b .
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Fantastic!!!
To simplify this, you could notice that 2 sin(x) cos(x) = sin(2x). So the integral is simplified to v^2*sin(2x)/g
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First we must consider the fact that the probability of choosing some angle θ between 0 and 2 π is completely uniform. The same goes for choosing some velocity v between 0 and v m a x . We calculate a probability density function for choosing a ( θ , v ) pair by realizing that P ( θ , v ) = C , where C is some constant:
∫ 0 v m a x ∫ 0 π / 2 C d θ dv = C ∫ 0 v m a x 2 π dv = C 2 π v m a x = 1 ⇒ C = π v m a x 2
Notice how I set the integral equal to one, as the probability density function has to be normalized. Next, we have to set up the following equations:
x = v t cos θ y = v t sin θ − 2 1 g t 2
From these equations, we can easily get:
t = t cos θ x ⇒ y = t cos θ x v sin θ − 2 1 g ( t cos θ x ) 2 = x tan θ − 2 v 2 cos 2 θ g x 2
Since we are interested in range, we can set y = 0 and create a function of the form x ( v , θ ) :
x tan θ − 2 v 2 cos 2 θ g x 2 = 0 ⇒ x tan θ = 2 v 2 cos 2 θ g x 2 ⇒ x = g 2 v 2 sin θ cos θ
We can now integrate the integral of this form to find the expectation value of our function:
⟨ x ⟩ = ∫ a b x P ( x ) dx = ∫ 0 v ∫ 0 π / 2 π v m a x 2 g 2 v 2 sin θ cos θ d θ dv = π v m a x 2 ∫ 0 v g 2 v 2 ∫ 0 π / 2 sin θ cos θ d θ dv
Now, using some simple u -substitution :
u = sin θ du = cos θ dx ⇒ ∫ 0 π / 2 u du = 2 u 2 ∣ ∣ ∣ ∣ 0 π / 2 = 2 sin 2 θ ∣ ∣ ∣ ∣ 0 π / 2 = 2 1
We can substitute this back into our original equation:
⇒ π v m a x 2 ∫ 0 v g 2 v 2 2 1 dv
Taking the remaining integral:
π v m a x 2 ∫ 0 v g 2 v 2 2 1 dv = π g v m a x 2 ∫ 0 v m a x v 2 dv = π g v m a x 2 3 v m a x 3 = 3 π g 2 v m a x 2
Looking the original question, the answer to the problem is given in the form a + b = 2 + 3 = 5 .
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Landing distance d = g 2 v 2 sin θ cos θ d a v = 2 π v max 1 ∫ 0 2 π ∫ 0 v max g 2 v 2 sin θ cos θ d v d θ = π g v max 4 ∫ 0 v max v 2 d v ∫ 0 2 π sin θ cos θ d θ = 3 π g 4 v max 2 ∫ 0 2 π sin θ cos θ d θ l e t u = sin θ d u = cos θ d θ d θ = cos θ d u d a v = 3 π g 4 v max 2 ∫ 0 1 u d u = 3 2 π g v max 2