Finding the Mass of a Helicopter

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SUMMARY

The mass of a helicopter can be determined by analyzing the forces acting on it when the main rotor blades, with a radius of 4.0 meters, push air downwards at a speed of 15 m/s. When the helicopter tilts forward at a 20-degree angle, it transitions from rising to accelerating horizontally at 3.57 m/s². The air density is given as 1.3 kg/m³, which is crucial for calculating the upward thrust generated by the rotor blades. The thrust must equal the weight of the helicopter at this point, allowing for the calculation of its mass.

PREREQUISITES
  • Understanding of momentum and center of mass concepts
  • Familiarity with basic physics equations related to force and thrust
  • Knowledge of trigonometric functions for calculating area reduction
  • Awareness of Betz's Law and its application in fluid dynamics
NEXT STEPS
  • Study the application of Betz's Law in calculating thrust from rotor blades
  • Learn how to apply the continuity equation in fluid dynamics
  • Explore the relationship between thrust, weight, and acceleration in helicopter dynamics
  • Investigate the effects of rotor blade angle on effective thrust generation
USEFUL FOR

Aerospace engineers, physics students, and anyone interested in helicopter dynamics and fluid mechanics will benefit from this discussion.

dydxx
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The question is:

The main rotor blades of a helicopter sweep out an area of radius 4.0m and push air downards with a speed of 15ms^(-1) away from the blades.

By tilting forwards 20 degrees, the helicopter stops rising and starts to accelerate horizontally at 3.57ms^(-2). The density of air is = 1.3kgm^(-3)..

Determine the mass of the helicopter?

We have been learning momentum and centre of mass and this was given as an extra question for homework but kinda confused how to approach it and also I am confused what relevant equations I should use as well. A push in the right direction would be amazing! :)
 
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outline of my thinking: cool problem!

The fundamental idea is that you have an area equivalent to that of the helicopter rotors with a radius of 4 meters pushing down air at the stated density. That gives you a force up. This assumption eliminates the need to fuss with the varying rotational speed along the rotors and likely a varying radial shape along the length as well.

I think what the problem implies is that at a reduction in downward force caused by a 20% incline of the rotors, the thrust up is reduced to just offset, that is equal, the weight[mass] of the helicopter...it stops rising and starts moving horizontally. So how much is the area effectively reduced when the rotors are inclined...I'd pick a trig function reflecting that reduction... either area or radius...which do you think?

If you buy that description, or have another interpretation,proceed along with this:
https://en.wikipedia.org/wiki/Betz'...onservation_of_mass_.28continuity_equation.29
 

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