Projectile motion with aerodynamic drag

In summary: cho mentioned that the projectile would reach its maximum altitude and horizontal distance if there was no aerodynamic drag.
  • #1
guywinford
2
0
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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  • #2
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]
 
  • #3
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.
 
  • #4
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
 

1. What is projectile motion with aerodynamic drag?

Projectile motion with aerodynamic drag is the motion of an object, such as a ball or a rocket, that is propelled through the air and experiences the resistance of air molecules. This resistance, known as aerodynamic drag, affects the trajectory and speed of the object as it moves through the air.

2. How does aerodynamic drag affect projectile motion?

Aerodynamic drag is a force that acts opposite to the direction of motion of an object, slowing it down. This means that an object experiencing aerodynamic drag will have a shorter and lower trajectory compared to an object without drag. Additionally, the greater the speed of the object, the greater the aerodynamic drag force acting upon it.

3. How is aerodynamic drag calculated in projectile motion?

The aerodynamic drag force can be calculated using the drag equation, which takes into account the density of the air, the object's velocity, its cross-sectional area, and a drag coefficient that depends on the shape and surface of the object. This equation allows for the prediction of the amount of drag force acting on a projectile at a given speed.

4. How does air density affect projectile motion with aerodynamic drag?

Air density, which is influenced by factors such as altitude, temperature, and humidity, affects projectile motion with aerodynamic drag by altering the amount of air molecules that the object encounters. A higher air density means more molecules for the object to collide with, resulting in a greater drag force and a shorter range.

5. Can aerodynamic drag be reduced in projectile motion?

Aerodynamic drag can be reduced in projectile motion by altering the shape and surface of the object to minimize its drag coefficient. Additionally, increasing the object's speed can create a "lift" force that counteracts the drag force, allowing for a longer and higher trajectory. However, it is impossible to completely eliminate aerodynamic drag in projectile motion.

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