How Do You Calculate the Range of a Cannon Ball on an Inclined Plane?

Gogsey
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1. A cannon mounted on a inclined plane launches a ball with initial speed v0 directly up the slope. The plane is inclined at angle phi above the horizontal, and the initial velocity is at angle theta above the plane. Using axes with x parallel to the plane and y normal to it, write out the x and y components of Newton’s second law, and show that the ball lands on the slope a distance R = (2V(o)^2 sin(theta) coa(theta + phi))/(g cos^2(phi)) from the cannon.

I can almost get the direction equations as required from the first part, but all these sin Phi, cos Phi, sin theta, and cos theta terms are confusing me.

Also, once you have these equations I'm kinda lost as what to do to get the distance R.

Thanks
 
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Post the working that you've done so far. You need to show attempt of some kind first.
 
I know the equations are:

x = Vot(cos (theta)) + 1/2 gt^2(sin(phi))

y = Vot(sin (theta)) + 1/2 gt^2(cos(phi))

Trouble is I don't know how to get them. I started off by integrating ax and ay to get vx and vy, and then again ro get dx and dy. But its the angles I'm confused about.

Shouldn't the y component always be sine, and the x component be cos? Plus I'm not sure if the x component is exactly up the incline, and y component perpenddicular to the surface, because that's the way the axis are pointing. Doen't that mean the x compnent should only have theta in the equation, because that's the angle between the inclined plane and the projectile?

I think I now get why phi is in the terms with g and theta is in the terms with Vo, since the y component is angle phi with gravity, amf x component is theta to the incline. Still just a little confused about where the sin and cos shoulgd go in each equation, ie in the first or second terms.

I'm really not sure how to start the seond part still.
 
Anyone?
 
If you show your expressions for a_x and a_y and what you got when you integrated them, I'll be able to see where you are going wrong an help you.
 
Normally, I would say that ay=-g and that ax=0, but If you start with zero accelaration, you can't get the same expression for X.
 
Gogsey said:
Normally, I would say that ay=-g and that ax=0

But gravity points downward. Is the negative y-direction really downward? Don't you have to take into account the angle of the plane?:wink:
 
ax=gcoes(phi), and ay=gsin(phi), then Vx=gtcos(phi), and vy=gtsin(phi). Finally, x=vot(cos(angle)=(1/2)gt^2(cos(phI), and y=vot(sin(angle)+1/2gt^2sin(phi).

I believe "angle" is theta since that's the angle ox of the projectile with the rotated plane.
 
Gogsey said:
ax=gcoes(phi), and ay=gsin(phi)
Good :smile: Of course, this assumes that g is negative right? (g=-9.8m/s2)

, then Vx=gtcos(phi), and vy=gtsin(phi).

Why aren't there any constants of integration?

Finally, x=vot(cos(angle)=(1/2)gt^2(cos(phI), and y=vot(sin(angle)+1/2gt^2sin(phi).

This does not follow from your previous expressions. :confused:
 
  • #10
Sorry, I'm so used to them not being important that I forget a lot of the time.

Yeah, I've got cos and sin the wrong way round fpr th vot terms. Not sure why its the other way round though?
 
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  • #11
Include them and use your initial conditions to determine them :smile:
 
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