Helicopter and Kinematics Problem

In summary: I just typed numbers...sorry.In summary, the height of a helicopter above the ground was given by h=2.90t^3, where h is in meters and t is in seconds. After 1.80 s, the helicopter released a small mailbag which reached a maximum height of 16.9 m from the ground. The velocity of the mailbag at release was 18.8 m/s, which was equal to the velocity of the helicopter at the time of release. The velocity of the mailbag when it hit the ground was -18.2 m/s. It took approximately 3.12 seconds for the mailbag to reach the ground after its release. Using kinematic equations and differentiation, these values
  • #1
intriqet
21
0

Homework Statement



The height of a helicopter above the ground is given by h=2.90t^3, where h is in meters and t is in seconds. After 1.80 s, the helicopter releases a small mailbag. Assume the upward direction is positive and the downward direction is negative.

A) what is the velocity of the mailbag when it is released?
B) What max height from the ground does the mailbag reach?
C) What is the velocity of the mailbag when it hits the ground?
D) How long after its release does the mailbag reach the ground?


Homework Equations



Kinematic equations



The Attempt at a Solution



So for the first part shouldn't the velocity at release be zero? if not what time interval would I use to derive velocity at release?

Also, max height should be 2.90(1.80)^3 = 16.9 m

if part a is zero then the final velocity can be derived by equation Vf^2 - Vi^2 = 2a * deltaX.
= -18.2 m/s

the velocity

However, the online service won't accept my answer. :/
 
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  • #2
would the velocity be zero? the helicopter is moving up, right?

it gives you the formula;

h = 2.6 t^3 which you could also say x = 2.6 t^3

does this look familiar? think about differentiation.

what's the change of displacement with respect to time? (in this case) ([tex]\frac{dx}{dt}[/tex])

from that you can work out it's velocity at release.

just a hint but you might also think, maybe the helicopter is accelerating upwards? it's not a very linear relationship is it? :eek: so try to think about that as well

(hint: [tex]\frac{d^2 x}{dt^2}[/tex])
 
  • #3
intriqet said:
So for the first part shouldn't the velocity at release be zero? if not what time interval would I use to derive velocity at release?
No, velocity at release would be equal to the velocity of the helicopter at the time of release.
[tex]v = \frac{dh}{dt}[/tex]
 
  • #4
2.9t^3 dh/dt = 5.8t^2

V-heli at 1.80 sec = 18.8 m/s = Vi-package which Webassign will not accept.

please help and thanks for the quick reply!
 
  • #5
2.9 * 3 isn't 5.8! =P
 
  • #6
Oh i knew that...lol sorry I was in a rush to go to class
 

Related to Helicopter and Kinematics Problem

1. What is a helicopter?

A helicopter is a type of aircraft that is lifted and propelled by rotating blades, also known as rotors. It is able to fly up, down, forward, backward, and hover in place due to the movement and control of its rotors.

2. How do helicopters fly?

Helicopters fly by using the lift generated by the rotation of their rotor blades. The rotor blades are able to change pitch and angle, allowing the helicopter to move in different directions and maintain its stability in the air.

3. What is the principle behind helicopter flight?

The principle behind helicopter flight is based on Newton's Third Law of Motion, which states that for every action, there is an equal and opposite reaction. The rotation of the rotor blades creates lift, while the air moving in the opposite direction provides an equal and opposite force to keep the helicopter in the air.

4. How is the speed of a helicopter measured?

The speed of a helicopter is typically measured in knots, which is a unit of speed used in aviation. It is equivalent to one nautical mile per hour. The speed of a helicopter can also be measured in miles per hour or kilometers per hour.

5. What factors affect the flight of a helicopter?

Several factors can affect the flight of a helicopter, including air density, altitude, temperature, wind speed and direction, weight and balance of the helicopter, and the design and condition of the rotor blades. These factors can impact the performance, stability, and maneuverability of the helicopter.

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