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Question: Two points A and B are located on the ground a certain distance $10\sqrt{2}$ m apart. Two rocks are ...

Two points A and B are located on the ground a certain distance 10210\sqrt{2} m apart. Two rocks are launched simultaneously from points A and B with equal speeds but at different angles. Each rocks lands at the launch point of the other. Knowing that one of the rocks is launched at an angle θ=37\theta = 37^\circ with the horizontal, what is the minimum distance between the rocks during the flight? (given: cos37° = 4/5)

A

2 m

B

4 m

C

6 m

D

8 m

Answer

2 m

Explanation

Solution

The problem describes a scenario of projectile motion where two rocks are launched simultaneously from points A and B, with a distance R=102R = 10\sqrt{2} m between them. Both rocks are launched with the same initial speed v0v_0 but at different angles. Crucially, each rock lands at the launch point of the other. This implies that the horizontal range of both projectiles is equal to the distance RR.

Let the launch angles be θ1\theta_1 and θ2\theta_2. The horizontal range RR of a projectile launched with speed v0v_0 at an angle θ\theta is given by the formula: R=v02sin(2θ)gR = \frac{v_0^2 \sin(2\theta)}{g}

Since both rocks have the same range RR and the same initial speed v0v_0, we have: v02sin(2θ1)g=v02sin(2θ2)g\frac{v_0^2 \sin(2\theta_1)}{g} = \frac{v_0^2 \sin(2\theta_2)}{g} This simplifies to sin(2θ1)=sin(2θ2)\sin(2\theta_1) = \sin(2\theta_2). Given that the angles are different, the relationship between them must be 2θ1=1802θ22\theta_1 = 180^\circ - 2\theta_2, which leads to θ1+θ2=90\theta_1 + \theta_2 = 90^\circ.

We are given that one of the rocks is launched at an angle θ1=37\theta_1 = 37^\circ. Therefore, the other launch angle is θ2=9037=53\theta_2 = 90^\circ - 37^\circ = 53^\circ.

We are also given cos(37)=4/5\cos(37^\circ) = 4/5. From this, we can deduce sin(37)=1(cos(37))2=1(4/5)2=116/25=9/25=3/5\sin(37^\circ) = \sqrt{1 - (\cos(37^\circ))^2} = \sqrt{1 - (4/5)^2} = \sqrt{1 - 16/25} = \sqrt{9/25} = 3/5. Using the complementary angle identities, sin(53)=cos(37)=4/5\sin(53^\circ) = \cos(37^\circ) = 4/5 and cos(53)=sin(37)=3/5\cos(53^\circ) = \sin(37^\circ) = 3/5.

Now, let's set up a coordinate system. Let point A be the origin (0, 0) and point B be at (R,0)(R, 0).

The position of the rock launched from A (Rock 1) at time tt is: x1(t)=v0cos(θ1)t=v0cos(37)t=45v0tx_1(t) = v_0 \cos(\theta_1) t = v_0 \cos(37^\circ) t = \frac{4}{5} v_0 t y1(t)=v0sin(θ1)t12gt2=v0sin(37)t12gt2=35v0t12gt2y_1(t) = v_0 \sin(\theta_1) t - \frac{1}{2}gt^2 = v_0 \sin(37^\circ) t - \frac{1}{2}gt^2 = \frac{3}{5} v_0 t - \frac{1}{2}gt^2

The rock launched from B (Rock 2) starts at (R,0)(R, 0) and travels towards A. Its position at time tt is: x2(t)=Rv0cos(θ2)t=Rv0cos(53)t=R35v0tx_2(t) = R - v_0 \cos(\theta_2) t = R - v_0 \cos(53^\circ) t = R - \frac{3}{5} v_0 t y2(t)=v0sin(θ2)t12gt2=v0sin(53)t12gt2=45v0t12gt2y_2(t) = v_0 \sin(\theta_2) t - \frac{1}{2}gt^2 = v_0 \sin(53^\circ) t - \frac{1}{2}gt^2 = \frac{4}{5} v_0 t - \frac{1}{2}gt^2

The time of flight for Rock 1 is T1=2v0sin(θ1)g=2v0(3/5)g=6v05gT_1 = \frac{2v_0 \sin(\theta_1)}{g} = \frac{2v_0 (3/5)}{g} = \frac{6v_0}{5g}. The time of flight for Rock 2 is T2=2v0sin(θ2)g=2v0(4/5)g=8v05gT_2 = \frac{2v_0 \sin(\theta_2)}{g} = \frac{2v_0 (4/5)}{g} = \frac{8v_0}{5g}. Since T1<T2T_1 < T_2, both rocks are in flight during the interval [0,T1][0, T_1].

We are interested in the distance between the rocks. Let's find the difference in their coordinates: Δx(t)=x1(t)x2(t)=45v0t(R35v0t)=(45+35)v0tR=75v0tR\Delta x(t) = x_1(t) - x_2(t) = \frac{4}{5} v_0 t - (R - \frac{3}{5} v_0 t) = (\frac{4}{5} + \frac{3}{5}) v_0 t - R = \frac{7}{5} v_0 t - R Δy(t)=y1(t)y2(t)=(35v0t12gt2)(45v0t12gt2)=(3545)v0t=15v0t\Delta y(t) = y_1(t) - y_2(t) = (\frac{3}{5} v_0 t - \frac{1}{2}gt^2) - (\frac{4}{5} v_0 t - \frac{1}{2}gt^2) = (\frac{3}{5} - \frac{4}{5}) v_0 t = -\frac{1}{5} v_0 t

The square of the distance between the rocks is d(t)2=(Δx(t))2+(Δy(t))2d(t)^2 = (\Delta x(t))^2 + (\Delta y(t))^2: d(t)2=(75v0tR)2+(15v0t)2d(t)^2 = (\frac{7}{5} v_0 t - R)^2 + (-\frac{1}{5} v_0 t)^2 d(t)2=(4925v02t2275v0tR+R2)+125v02t2d(t)^2 = (\frac{49}{25} v_0^2 t^2 - 2 \cdot \frac{7}{5} v_0 t R + R^2) + \frac{1}{25} v_0^2 t^2 d(t)2=5025v02t2145v0Rt+R2d(t)^2 = \frac{50}{25} v_0^2 t^2 - \frac{14}{5} v_0 R t + R^2 d(t)2=2v02t2145v0Rt+R2d(t)^2 = 2 v_0^2 t^2 - \frac{14}{5} v_0 R t + R^2

This is a quadratic equation in tt of the form at2+bt+cat^2 + bt + c, where a=2v02a = 2v_0^2, b=145v0Rb = -\frac{14}{5} v_0 R, and c=R2c = R^2. The minimum value of this quadratic occurs at tmin=b/(2a)t_{min} = -b/(2a). tmin=(145v0R)/(22v02)=14v0R54v02=14R20v0=7R10v0t_{min} = -(-\frac{14}{5} v_0 R) / (2 \cdot 2 v_0^2) = \frac{14 v_0 R}{5 \cdot 4 v_0^2} = \frac{14 R}{20 v_0} = \frac{7R}{10 v_0}

To ensure this minimum occurs during the flight, we compare tmint_{min} with T1T_1. We need to find v0v_0. The range RR is given by R=v02sin(2θ1)gR = \frac{v_0^2 \sin(2\theta_1)}{g}. 102=v02sin(2×37)g=v02sin(74)g10\sqrt{2} = \frac{v_0^2 \sin(2 \times 37^\circ)}{g} = \frac{v_0^2 \sin(74^\circ)}{g} sin(74)=2sin(37)cos(37)=2×(3/5)×(4/5)=24/25\sin(74^\circ) = 2 \sin(37^\circ) \cos(37^\circ) = 2 \times (3/5) \times (4/5) = 24/25. So, 102=v02(24/25)g10\sqrt{2} = \frac{v_0^2 (24/25)}{g}, which means v02g=102×2524=250224=125212\frac{v_0^2}{g} = \frac{10\sqrt{2} \times 25}{24} = \frac{250\sqrt{2}}{24} = \frac{125\sqrt{2}}{12}.

Now, let's express T1T_1 in terms of RR and v0v_0: T1=6v05gT_1 = \frac{6v_0}{5g}. We can write g=v02(24/25)Rg = \frac{v_0^2 (24/25)}{R}. T1=6v05(v02(24/25)R)=6v0R5v02(24/25)=6R5v0(24/25)=6Rv0(120/25)=6Rv0(24/5)=30R24v0=5R4v0T_1 = \frac{6v_0}{5 \left(\frac{v_0^2 (24/25)}{R}\right)} = \frac{6v_0 R}{5 v_0^2 (24/25)} = \frac{6R}{5 v_0 (24/25)} = \frac{6R}{v_0 (120/25)} = \frac{6R}{v_0 (24/5)} = \frac{30R}{24v_0} = \frac{5R}{4v_0}.

Comparing tmint_{min} and T1T_1: tmin=7R10v0t_{min} = \frac{7R}{10v_0} T1=5R4v0=12.5R10v0T_1 = \frac{5R}{4v_0} = \frac{12.5R}{10v_0} Since 7R10v0<12.5R10v0\frac{7R}{10v_0} < \frac{12.5R}{10v_0}, the minimum distance occurs within the flight time of both rocks.

Now, substitute tmint_{min} back into the equation for d(t)2d(t)^2: dmin2=2v02(7R10v0)2145v0R(7R10v0)+R2d_{min}^2 = 2 v_0^2 (\frac{7R}{10 v_0})^2 - \frac{14}{5} v_0 R (\frac{7R}{10 v_0}) + R^2 dmin2=2v0249R2100v0298R250+R2d_{min}^2 = 2 v_0^2 \frac{49R^2}{100 v_0^2} - \frac{98 R^2}{50} + R^2 dmin2=98R210098R250+R2d_{min}^2 = \frac{98 R^2}{100} - \frac{98 R^2}{50} + R^2 dmin2=49R25098R250+50R250d_{min}^2 = \frac{49 R^2}{50} - \frac{98 R^2}{50} + \frac{50 R^2}{50} dmin2=(4998+50)R250=1R250d_{min}^2 = \frac{(49 - 98 + 50) R^2}{50} = \frac{1 R^2}{50}

The minimum distance dmind_{min} is the square root of dmin2d_{min}^2: dmin=R250=R50=R52d_{min} = \sqrt{\frac{R^2}{50}} = \frac{R}{\sqrt{50}} = \frac{R}{5\sqrt{2}}

Finally, substitute the given value of R=102R = 10\sqrt{2} m: dmin=102 m52=2 md_{min} = \frac{10\sqrt{2} \text{ m}}{5\sqrt{2}} = 2 \text{ m}

The minimum distance between the rocks during the flight is 2 m.