(projectile motion) calculation problem

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SUMMARY

The discussion centers on calculating the length of OA for a ball thrown from an inclined plane with angles φ and θ. The initial equations derived include x = V₀cos(φ)t and y = V₀sin(φ)t - 0.5gt², leading to the time of flight t = [2V₀sin(φ-θ)]/[gcos(θ)]. The correct expression for OA is established as OA = V₀²*[sin(2φ-θ) - sin(θ)]/[gcos²(θ)]. Participants clarify the derivation steps and emphasize the importance of trigonometric identities in reaching the maximum value of OA.

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asdf1
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Question: A ball with a velocity of Vo is thrown from the bottom of an inclined plane (point O) with an angle of \phi. The inclined plane has an angle oftheta . The ball lands on top of the inclined plane on a point A. Find the length of OA and its maximum value.

My calculations:
1. x = V_{0}\cos (\phi) t
2. y=Vo*sin\phit -0.5*gt^2
3. y=xtan\theta

From the above equations, I got t=[2Vo*sin(\phi-\theta)/[gcos\theta]
So OA= xsec\theta
=Vo*cos\phi*sec\theta/(gcos\theta)

But the answer is
OA= Vo^2*[sin(2\phi-\theta)-sin\theta]/[gcos^2(\theta)]

And I don't know how to tell from my calculations what the max value is, and why it's different from the answer...
Can somebody help?

http://img97.imageshack.us/my.php?image=inclinedplanesu8.png"
 
Last edited by a moderator:
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Change your tags to [ tex ] ... [ /tex ] (without the spaces obviously) :wink:

Click on this equation below to see how it is coded;

x = V_{0}\cos (\phi) t
 
Last edited:
thanks for teaching me latex! ^_^
 
asdf1 said:
1. x = V_{0}\cos (\phi) t
2. y=Vo*sin\phit -0.5*gt^2
3. y=xtan\theta

From the above equations, I got t=[2Vo*sin(\phi-\theta)/[gcos\theta]
How did you arrive at this? Would you mind posting your steps?
 
from 1. and 3. ->
y=V_{0}\cos (\phi) t*tan\theta
then take the above result and plug it into 2. getting:
y=Vo*sin\phit -0.5*gt^2=V_{0}\cos (\phi) t*tan\theta

Rearranging the equation and using the formula
sin2\phi=2sin\phicos\phi to simplfy the equation makes the result for
t=[2Vo*sin(\phi-\theta)/[gcos\theta]
 
asdf1 said:
From the above equations, I got t=[2Vo*sin(\phi-\theta)/[gcos\theta]
So OA= xsec\theta
Up to this point, everything is fine.
asdf1 said:
OA=Vo*cos\phi*sec\theta/(gcos\theta)
You seem to have made an error here. What is the expression for x?
 
Last edited:
Sorry! I mistyped!
It should be
OA= Vo*cos\phi*2Vo*sin(\phi-\theta)*sec\phi/[gcos\phi]
 
asdf1 said:
OA= Vo*cos\phi*2Vo*sin(\phi-\theta)*sec\phi/[gcos\phi]

Do you mean OA= Vo*cos\phi*2Vo*sin(\phi-\theta)*sec\theta/[gcos\theta]?

If yes, then you are on the right track. Compare your answer with the one given in the book. What is the last step you need to take?
 
Last edited:
Yes...
I think that I have to use some kind of trignometric formula to get the answer in the book?
 
  • #10
the ans should come out to be
R=(2u<sq (only u)>sin<sq>(a-b)cos<sq>a)/(gcosb)<sq>

the max value will be when a= 45-b/2

where a = angle of projection + angle of inclination(b)
angle of inclination=b

if u ask i will mail u the proof
 
  • #11
A Better solution

Hello
well i have written a different solution
i am taking axis along the incline and perpendicular to the incline then taking components of g(acceleration due to gravity) along and perpendicular to the incline and then applying kinematics equations
anywayshttp://helpjee.blogspot.com/2006/08/inclined-plane-problem_01.html"
bye
:smile: :smile:
 
Last edited by a moderator:
  • #12
Wow! thank you for the different approach!
 

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