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#1 2010-06-13 13:55:17

jinx007
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Registered: 2010-06-13
Posts: 1

dynamics

Dynamics question please help i am stuck...!  sadsad

A model helicopter of mass 5.0 kg rises with constant acceleration from rest to a height of 60 m in 10 seconds. Find the thrust exerted by the rotor blades during the ascent.

The answer in the book is 55 N

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#2 2010-06-20 08:42:52

Astro
Member
Registered: 2010-05-03
Posts: 113

Re: dynamics

Ok, i won't do this for you, you can work it out, but i can help.

Thrust is simply a force, just like weight, and this is in 55 Newtons then a solution.

So weight and gravity can be taken into account, including the gravitational potential and height.

working with a constant acceleration makes things a lot easier, so you know the mass - a constant acceleration can be appliable to the equation of motion:

F=Ma

Since we have a height involved, we also have the idea of kinetic energy and potential energy - in your condition, your object began stationary, so it's height from the ground must began as:

gh=v*^2 because v=0 and g is the gravitational acceleration. From this, we find the height equation given as -\frac{h}{2}= \frac{v*^2 - v^2}{-2g} states that something is \frac{h}{2} units from the ground. To find the work done for the force of thrust, one might also want to use the equation W_k=Fh which is the work due to the kinetic energy, so equally W_k=mgh because GPE=Wh where GPE is the gravitational potential energy and W is the work, and inversely related also is the height h.

So for any object which for arguements sake has a force applied where the acceleration is an upwards motion, the unit of the gravitational potential energy is the same measurement of the work done; so we must apply it an amount of potential energy equal to the work applied to it to begin with.

Last edited by Astro (2010-06-20 08:44:39)

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#3 2010-06-20 08:49:32

Astro
Member
Registered: 2010-05-03
Posts: 113

Re: dynamics

You can read this as well which should show you generally how to get around your problem. Good luck! http://my.execpc.com/~culp/rockets/applied.html

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