Calculating Thrust for a 1.5 HP Motor: Tips for Project Hovercraft

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In summary, the conversation discusses the calculation of vertical thrust for a 1.5 horsepower motor in order to lift 200 lbs in a hovercraft project. The speaker clarifies that thrust is not the relevant parameter for hovercrafts, as they work on pressure rather than reaction. The calculation involves considering the working surface, weight, pressure, and air leakage.
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Shane
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Does anyone know how to calculate the vertical thrust of 1.5 horsepower motor? I need some calculations for a project hovercraft and am wondering how much thrust is needed to lift 200 lbs. Also is thrust affected by fan blade size? Any help is appreciated, Thanks!
 
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Well to start with a hovercraft doesn't work on the reaction principle like a rocket does, so thrust isn't the relevant parameter of merit. They work by pressure. If your hovercraft is on a very smooth surface you can get by with a small amount of power, but in real life they need quite a lot of power to overcome the leakage associated with rough surfaces. So you need to calculate the working surface of the hovercraft, the weight, the working pressure and the rate of leakage of air past the base for a given height. Then you will be able to calculate the power needed.
 
  • #3


Calculating the thrust for a 1.5 horsepower motor for a project hovercraft can be done by using the formula: Thrust (lbs) = (Horsepower x 550) / Velocity (ft/min). In this case, the velocity would be the speed of the fan blades in feet per minute.

To lift 200 lbs, you would need a thrust of at least 200 lbs. However, it is recommended to have a higher thrust to account for any additional weight or resistance.

The fan blade size can affect the thrust as it determines the amount of air that can be moved per rotation. A larger fan blade size can generate more thrust, but it also requires more power from the motor.

Another factor that can affect thrust is the design and shape of the fan blades. A more efficient design can generate more thrust with the same amount of power.

Overall, it is important to consider the power and efficiency of the motor, as well as the design of the fan blades, when calculating the thrust for your project hovercraft. It is also recommended to do some testing and adjustments to fine-tune the thrust for optimal performance.
 

Related to Calculating Thrust for a 1.5 HP Motor: Tips for Project Hovercraft

1. What is thrust?

Thrust is a force that propels an object forward. In the context of physics and engineering, it refers to the force that is produced by a propulsion system, such as a rocket engine or a jet engine.

2. How is thrust calculated?

Thrust can be calculated using the equation: T = m * a, where T is thrust, m is the mass of the object, and a is the acceleration. However, in the case of a propulsion system, other factors such as the velocity of the exhaust gases and the efficiency of the engine also need to be taken into account.

3. What units are used to measure thrust?

Thrust is typically measured in units of force, such as Newtons (N) or pounds (lbs). In the context of rocket engines, thrust is often measured in pounds of force (lbf) or in kN (kilonewtons).

4. How does thrust affect an object's motion?

Thrust is a force that acts in the opposite direction of an object's motion. When thrust is greater than the opposing forces, such as air resistance, the object will accelerate and move in the direction of the thrust. However, if the opposing forces are greater, the object will decelerate or even move in the opposite direction.

5. Are there any limitations to calculating thrust?

Calculating thrust can become more complex when dealing with real-world scenarios, as there are many factors that can affect the actual thrust produced by a propulsion system. Factors such as air density, temperature, and altitude can all impact the performance of an engine and therefore the thrust it produces. Additionally, thrust can also vary over time as the engine's fuel burns and its weight changes. These variables make it challenging to accurately calculate thrust in practical applications.

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