Projectile motion with aerodynamic drag

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Homework Help Overview

The problem involves analyzing the motion of a projectile launched at an angle with an initial speed, while considering the effects of aerodynamic drag. The objective is to determine the maximum altitude and horizontal distance traveled by the projectile, with specific parameters provided for mass, angle, initial speed, and drag coefficient. A comparison to the scenario without drag is also requested.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning, Problem interpretation

Approaches and Questions Raised

  • Participants discuss using Newton's 2nd Law to analyze vertical acceleration at maximum height, noting that vertical velocity is zero at that point. Others suggest splitting the problem into horizontal and vertical components and setting up equations for forces in both directions. There is mention of needing to use computational tools for solving the problem, reflecting uncertainty about starting points and methods.

Discussion Status

The discussion is ongoing, with various approaches being explored. Some participants have provided insights into setting up the equations of motion, while others express uncertainty about how to begin. There is no explicit consensus on a single method, but guidance has been offered regarding the use of component analysis and integration.

Contextual Notes

Participants note the complexity introduced by aerodynamic drag and the potential need for numerical methods or software to solve the equations, indicating that analytical solutions may be challenging. The problem's constraints and parameters are clearly defined, but the discussion reflects a range of interpretations and approaches.

guywinford
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here's the problem:

A projectile of mass "m" is launched from ground level at an angle of "theta" above the horizontal and with an initial speed "v". The flight of the projectile is resisted by an aerodynamic drag force modeled as uv^2, where "v" is the speed of the projectile and "u" is the drag coefficient.

Find the maximum altitude "h" reached by the projectile and the horizontal distance "d" it travels before striking the ground.

Let m=5 kg; theta=45 degrees; v=200 m/s; and u=100x10^-6 kg/m

Compare answer to the case of no aerodynamic drag.

any help would be great
 
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Use Newton's 2nd Law at Max height to determine its vertical acceleration.
Remember Vy is 0 at max height, so there will be left only Vx at this point.

[tex]\sum F_{y} = ma[/tex]
 
i really don't know where to start with this problem but i do know that a computer program or excel must be used to solve it.
 
The way I would approach this problem is such:
(I won't put all the working, but hopefully will explain it enough)

I would split the problem into components x and y.

So:

[tex]F_x = -uv_x^2 = ma = m\frac{dv_x}{dt}[/tex]

and:

[tex]F_y = -uv_y^2 - mg = ma = m\frac{dv_y}{dt}[/tex]

you can solve these for [itex]v_x and v_y[/itex] in terms of t.

Don't forget your integration constants!
(remember that at t=0

[tex]v_x = v_0 cos(\theta) and v_y = v_0 sin(\theta)[/tex]

You also know that :


[tex]\frac{dx}{dt} = v_x and \frac{dy}{dt}= v_y[/tex]

so you can solve for x and y by integration.

as cycl said, v_y = 0 at max height -> you can then solve your v_y equation for t, and substitute this t value into your y equation to get the max height.

For the max range, y = 0. Solve your y equation for t, then substitute that into your x equation.

Alternatively you can find x in terms of y for the general case but
the algebra can get bit nasty with this problem, linear drag is much nicer.

Hope that helps,

give us a yell if it doesn't

Ty
 

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