Finding the Launch Angle of an Artillery Gun

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SUMMARY

The discussion focuses on calculating the launch angle for an artillery gun to hit a target 12.5 km away when fired at a velocity of 650 m/s, assuming negligible air resistance. The key equations used include the projectile motion equations, specifically the horizontal and vertical components of velocity, and the time of flight derived from these components. The final solution involves substituting the time of flight into the vertical motion equation to solve for the angle θ, ultimately leading to a successful calculation of the launch angle.

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kvan
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Homework Statement



An artillery gun is trying to hit a target that is 12.5 km away. If the shell is fired at 650 ms-1 at what angle above the horizontal should the gun be fired to hit the target assuming that air resistance is negligible? [g=9.8 ms-2]

Homework Equations



I tried using v^2_y = v^2_0_y + 2gt and v_x = \frac{d_x}{t}

The Attempt at a Solution



I tried breaking the 650m/s into component vectors for x and y. I used the y component to try and find time it took to reach maximum height, then doubled this value to find total time. I used this value for time and plugged it into v=d/t in an attempt to maybe create an equation where I could find the angle for the cannon.

I got stuck at that point and I don't really know what to do. Any suggestions?
 
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Hi kvan, welcome to PF.

Your approach is correct. Show your calculations.
 
Thanks, well my component vectors look like this

y= 650\sin\theta
x= 650\cos\theta

I use the y value and plugged it into

v^2_y= v^2_0_y + 2gt

rearranged into

\frac {t = v^2_y - v^2_0_y}{2g}
\frac {0^2 - (650\sin\theta)^2}{-9.8*2}

since this value for t is just the time taken to reach maximum height I doubled it giving me

\frac {(650\sin\theta\)^2} {9.8}

I tried to simplify the value so I squared the 650 and divided by 9.8

43112(\sin\theta)^2

I then used the equation

v_x = \frac {d_x}{t}

which gives me

650\cos\theta = \frac{12500}{43112(\sin\theta)^2}

I had converted the 12.5km to 12500m. I attempt to move all the values of \theta to one side

\cos\theta\ = \frac{4.46*10^-4}{(\sin\theta)^2}

\cos\theta\*(\sin\theta\)^2 = 4.46*10^-4

I used trig identities to try and simplify the right side to only 1 trig function

\sin^2\theta = (\sin\theta)^2 = \frac{1-\cos 2\theta}{2}

I replace sin with cos

\cos\theta(\frac{1-\cos 2\theta}{2})=4.46*10^-^4

Multiply it through

\frac{\cos\theta - \cos^2 2\theta}{2} = 4.46*10^-^4

multiply both sides by 2

\cos\theta - \cos^2 2\theta =8.92*10^-^4

I factor out cos from the right side

\cos\theta (1-\cos 2\theta ) =8.92*10^-^4

That is basically all of my calculations. I get stuck at this point, any tips or pointers you guys can give?
Sorry if the math equations are hard to read, I'm kinda figuring out latex as I go along
 
Last edited:
Oh man, I can't believe I messed that up. I tried using the method you put but I don't think it works, or I did something wrong.

v_f_y = v_f_i - gt

0 = 650\sin\theta - 9.8t

t = \frac{650\sin\theta}{9.8}

T = 2t = 2* \frac{650\sin\theta}{9.8}

T = \frac {650\sin\theta}{4.9}

y=v_o\sin\theta*t-\frac{1}{2}gT^2

y=0

0=650\sin\theta*\frac{650\sin\theta}{4.9}-4.9*(\frac{650\sin\theta}{4.9})^2

=(\frac{650\sin\theta ^2}{4.9}) - (\frac{650\sin\theta ^2}{4.9})

I'm not really sure how to solve for the angle at this point since both sides equal each other. But did I make a mistake in my calculations?
 
In the problem range is given and the velocity is given. Then

Time of flight T = 12500m/650*cosθ.

Now y = Vo*sinθ*Τ - 1/2*g*T^2.

Put y = 0 and substitute the value of T and solve for θ.
 
I got the answer finally, thanks so much for the help. :D
 

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