Oblio
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well, my c = vsin(theta)
The discussion revolves around deriving the position of a projectile under the influence of gravity, specifically using Newton's second law. The original poster is attempting to integrate the equations of motion for a trajectory without air resistance, while also considering the implications of initial velocity and angles in the context of projectile motion.
The conversation is ongoing, with participants providing guidance on integrating the equations of motion and clarifying the roles of constants in the equations. There is a focus on ensuring the correct setup for both horizontal and vertical motion, and some participants are exploring how to eliminate time from the equations to express trajectory.
There is a mention of comparing trajectories with and without air resistance, and the problem requires deriving equations based on initial conditions that are not fully specified. Participants are also navigating the implications of different launch angles and initial velocities.
Oblio said:well, my c = vsin(theta)
Oblio said:D=0... ?
Oblio said:0 = ma
C=v(x)
v(x) =vcos(theta), C=Vcos(theta)
y=v(x)t +D
y=D
at t=0, D=0 also.
Oblio said:algebraically or through another situation such as (t=0) (not that one I realize though)
Oblio said:nope. lol
Oblio said:ok, it asks for the trajectory as a function of x so:
y=vsin(theta)x/cos(theta) - (1/2)g x^2/v^2cos(theta)^2
learningphysics said:there should be vcos(theta) in the denominator in the first term.
Oblio said:sorry.
had that in ink ( i promise!)
Oblio said:I actually did that FIRST, thinking I was doing part a, but I actually did b.
I think this question is basically done, I can show you my other section maybe?
They do basically match.
Oblio said:y= (v_{yo} + v_{ter}x) / v_{xo} + v_{ter}\tau ln (1 - x / v_{xo}\tau)
I'll skip a simplification step unless its needed: Used taylor's series which allowed cancellations.
y=v_{yo}x / v_{xo} - x^2v_{ter}\tau / 2v_{xo}^{2}\tau^{2}