Propeller rotating in horizontal plane

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Discussion Overview

The discussion revolves around the dynamics of a horizontally positioned propeller designed for a toy, specifically focusing on the airflow direction, thrust, and lift forces acting on the propeller after it is released. Participants explore the implications of these forces on the propeller's vertical ascent and horizontal movement.

Discussion Character

  • Exploratory
  • Technical explanation
  • Conceptual clarification

Main Points Raised

  • Some participants question whether the direction of airflow through the propeller is vertical, suggesting it has a rotational component and that real-world viscosity affects the surrounding air.
  • There is a discussion about thrust being responsible for vertical climb, while lift is proposed to cause horizontal movement, with lift defined as perpendicular to the airflow.
  • One participant notes that if the propeller is not perfectly vertical upon release, it will have a sideways component, leading to unbalanced aerodynamic forces that create horizontal movement.
  • Another participant mentions that the shape of the propeller blades may change due to centripetal and aerodynamic forces, which could further influence the aerodynamic forces acting on the propeller.
  • Clarification is provided that lift is defined relative to the airflow over the moving blades, suggesting it is nearly aligned with thrust in this context.

Areas of Agreement / Disagreement

Participants express varying views on the relationship between thrust and lift, and whether the propeller's behavior aligns with theoretical expectations. There is no clear consensus on the exact dynamics involved, particularly regarding the definitions and roles of thrust and lift in this scenario.

Contextual Notes

Participants acknowledge the complexity of the forces at play, including the effects of blade angle and material flexibility, which may not be fully resolved in their discussions. The relationship between thrust and lift remains a point of contention.

axe34
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Hello,

I have a project whereby I am designing a toy that spins a horizontally positioned propeller, then releases it.

After releasing it, the propeller gains height, but moves somewhat away from the operator of the toy.

Is the direction of airflow through the propeller vertically? If so, is it ''thrust'' that makes it climb and ''lift'' that makes it move forward? (lift is perpendicular to thrust).

Thanks
 
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axe34 said:
Is the direction of airflow through the propeller vertical?
The flow is mostly vertical with a rotational component. The ideal primary air flow diameter narrows as the speed of the air increases, but real world viscosity results in the surrounding air also being affected.

axe34 said:
If so, is it ''thrust'' that makes it climb and ''lift'' that makes it move forward? (lift is perpendicular to thrust).
Lift is perpendicular to the relative flow. For a propeller, "lift" would be perpendicular to the relative flow over a propeller blade, but the relative speed and direction of this flow is affected by the propeller, and the resulting induced flow speed and direction (rotation) changes somewhat depending on radial distance from the hub of the propeller.
 
Last edited:
axe34 said:
I have a project whereby I am designing a toy that spins a horizontally positioned propeller, then releases it.

After releasing it, the propeller gains height, but moves somewhat away from the operator of the toy.

Is that a description of what it does in real life, or a description of what you want it to do?

Initially the thrust force is along the axis of the prop. If the prop is not perfectly vertical when it is released, it will have a component that starts it moving sideways.

As soon as that happens, there is a relative "cross-wind" component of the incoming air, relative to the prop. That means the blades on one side of the prop have a higher speed relative to the air than the blades on the other side, so the aerodynamic forces are unbalanced and create a bigger horizontal force in some direction. The aero forces will also tend to rotate the prop to point in a different direction.

In helicopters, the angle of the blades is changed as they rotate, to control the forces generated by the rotor. In fixed wing aircraft, the relatively large inertia of the plane itself, and the other flight control surfaces, mean this effect from the propeller is not usually significant. And of course helicopters use the "sideways" component of force from the rotor to move horizontally relative the the ground, but fixed wing planes do not.

If the toy is made from flexible material, there is a further effect, in that the centripetal and aerodynamic forces on the blades will probably change their shape, and the change in shape will affect the aero forces. Understanding that in detail could make an interesting (and challenging) project!
 
I want the propeller to rise vertically, with minimal movement in the horizontal plane.

I'm required to draw free-body diagrams of the propeller in flight. I know that there will be a ''lift'' force that is defined to be perpendicular to the air flow.

If the thrust here is vertically upwards (or near enough), then I wonder if the ''lift'', which is defined to be perpendicular to airflow, is causing the prop to move away from the operator in the horizontal plane?
 
axe34 said:
''lift'', which is defined to be perpendicular to airflow ...
lift is perpendicular to the air flow relative to the moving blades of a propeller, so it's almost in the same direction as thrust.
 

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