Helicopter height and vertical speed?

Click For Summary
SUMMARY

The discussion centers on calculating the height of a 2500 kg helicopter accelerating upwards at 1.7 m/s² when its blades generate an upward force of 29 kN. The drag force was calculated using a turbulent drag coefficient of 0.45, resulting in a drag force of 4.5 kN. The vertical speed of the helicopter was determined to be 56 m/s, leading to a final height of 883 meters using the acceleration-velocity-distance formula. The calculations were critiqued for not consistently incorporating acceleration in all steps.

PREREQUISITES
  • Understanding of Newton's laws of motion
  • Familiarity with drag force calculations and coefficients
  • Knowledge of kinematic equations for motion
  • Basic principles of fluid dynamics
NEXT STEPS
  • Study the effects of drag on different shapes in fluid dynamics
  • Learn about the application of kinematic equations in real-world scenarios
  • Explore advanced topics in helicopter aerodynamics
  • Investigate the impact of varying drag coefficients on performance calculations
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in helicopter design or performance analysis will benefit from this discussion.

bbbl67
Messages
216
Reaction score
21

Homework Statement


This is not my homework question, I was asked to help with it, but I've been out of the engineering field for many years now. Here's the question:

Starting from rest, a 2500 kg helicopter accelerates straight up at a constant 1.7 m/s2. What is the helicopter's height at the moment its blades are providing an upward force of 29 kN? The helicopter can be modeled as a 2.6-m -diameter sphere, and air resistance is not negligible.

Homework Equations


Gravity:
F_g = m g

Drag:
C_d = F_d/(1/2 ρ u^2 A) |
F_d | drag force
C_d | drag coefficient
ρ | mass density
u | characteristic speed
A | frontal area

I looked up the drag coefficient (https://is.gd/qpe40K) of a sphere, and found two figures:
C_d = 0.1 (laminar)
C_d = 0.45 (turbulent)

So, I chose the turbulent figure (0.45).

The Attempt at a Solution


We know that the two forces will add up to 29 kN at a certain point, so:
F_g + F_d = 29 kN
F_d = 29 kN - F_g
= 29 kN - m g
= 29 kN - 2500 kg * 9.8 m/s^2
= 4.5 kN

The standard density of air at sea level is:
ρ = 1.204 kg/m^3

The frontal area of a sphere is:
A = pi * r^2
= pi * (2.6 m / 2)^2
= 5.309 m^2

So we have everything except the vertical speed of the helicopter, which we can find by rearranging the drag coefficient formula, and we get:
C_d = F_d/(1/2 ρ u^2 A)
u^2 = F_d/(1/2 ρ C_d A)
u = sqrt(F_d/(1/2 ρ C_d A))
= sqrt(4.5 kN/(0.5 * 1.204 kg/m^3 * 0.45 * 5.309 m^2))
= 56 m/s

Now to find the final height of the helicopter, we have to use and rearrange the acceleration-velocity-distance formula:

v_f^2 = v_i^2 + 2 a d |
v_f | final speed
a | acceleration
v_i | initial speed
d | distance

v_i = 0
v_f = u = 56 m/s
a = 1.7 m/s^2
d = h = ?
h = (v_f^2 - v_i^2)/ 2a
= (56 m/s)^2 / 2 (1.7 m/s^2)

Therefore,
h = 883 m

Were my procedures okay? Any critiques?
 
Physics news on Phys.org
bbbl67 said:
F_g + F_d = 29 kN
That would make the helicopter keep its speed.
Don't forget its acceleration.
 
mfb said:
That would make the helicopter keep its speed.
Don't forget its acceleration.
Well, the acceleration was used in the height calculation.
 
That is not the only step where you need it. I quoted the part where you forgot to consider it.
 

Similar threads

  • · Replies 1 ·
Replies
1
Views
2K
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 3 ·
Replies
3
Views
8K
  • · Replies 13 ·
Replies
13
Views
4K
  • · Replies 1 ·
Replies
1
Views
1K
  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 7 ·
Replies
7
Views
3K
  • · Replies 1 ·
Replies
1
Views
1K