Thrust calculation for hovercraft

In summary, the student is looking for information on how to calculate the power needed to make a light hovercraft go forward. They ask how to determine the acceleration that they expect and how to calculate the aerodynamic resistance. They are also looking for a good link.
  • #1
yablonski
4
0
hello to u all out there (sorry for the misspelling, english is not my native language)

i'm mechanical engineering student and I'm working on my final project which is design of a light hovercraft (acv).

i was wondering how do i calculate the power needed to make it go forward.??

do i need to determin the acceleration that i expect??

how do i derermine the aerodynamic resistens?

do u know w good link??

thanks ahead

yab
 
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  • #2
you need to determine the friction of the unit when it hovers. When i made it, i used the classical experiment:tongue: of determining the friction using a cord & putting weight on the other side of the pulley:rofl:.

this is the force you need to overcome. Use power = force*velocity to calculate the power at any velocity. note that the process is only approximate.

Forget about aerodynamic resistance, it will only complicate things, else use some correlations to calculate drag.
 
  • #3
hi again, i see now i left a part of your question. the force you calculated just above is to sustain the motion(non accelerating unit). If you need to reach some velocity in some time t(depends if the project have some objective), calculate the force by using F = m*a(inertia force).
 
  • #4
thank. the eq. power=f*velocity

what r the units of this "power"

isnt it supose to b power=pressure*volume of air?
 
  • #5
use SI units, power will be in J/s ot watts.

First power = pressure * volume flow rate, second is that there are a lot of variations of this equation, you can easily see it using dimensional analysis or using a differential element.

Third point is that if the objective of your query is to determine the thrust you require from the propeller, calculate the thrust usint the above equation & see some sites like thishttp://www.sharmamodelaero.com/propellers.htm. they ll have some graphs of thrust vs speed & type of motor required.
 
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  • #6
"Forget about aerodynamic resistance, it will only complicate things, else use some to calculate drag. "

which correlations do i use to avoid drag calculations??
 
  • #7
i remember that there are some in fluid mechanics, by fox & mcdonald.

Can you use fluent? or ansys? You can estimate the drag using FEA.
 

1. How is thrust calculated for a hovercraft?

Thrust for a hovercraft is calculated by multiplying the air flow rate by the difference in air pressure between the front and rear of the craft. This results in a force that propels the craft forward.

2. What factors affect the thrust of a hovercraft?

The main factors that affect the thrust of a hovercraft include the size and shape of the hovercraft, the type and power of the propulsion system, and the air cushion thickness.

3. How do you determine the appropriate amount of thrust for a hovercraft?

The appropriate amount of thrust for a hovercraft is determined by considering the weight of the craft, the desired speed and maneuverability, and the environmental conditions such as wind and water currents.

4. Can thrust be adjusted while a hovercraft is in motion?

Yes, thrust can be adjusted while a hovercraft is in motion. This is typically done through the control of the propulsion system, which can increase or decrease the amount of thrust being generated.

5. Are there any safety considerations when calculating thrust for a hovercraft?

Yes, safety should always be a top consideration when calculating thrust for a hovercraft. It is important to ensure that the craft is not generating too much thrust, as this can cause instability and difficulty in controlling the craft.

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