From theoretical airflow speed of rotating propeller to a realistic value?

In summary, the conversation discusses the calculation of volume flow of air generated by a static motor with a propeller attached. The formula used takes into account the prop pitch, diameter, and motor rpm, resulting in a theoretical airflow speed of 1000ft/min and a volume flow of 440 CFM. However, there may be other factors such as power consumption or a "ram air" factor that may affect the accuracy of this calculation. The speaker also mentions related questions they have on this topic.
  • #1
ash01
5
0
Hey,

Yet another propeller question on this board.
I have done my research, both here & on google, but I cannot seem to find an answer.

Lets say I have a motor on which I mount a propeller. This motor is static (not moving like on a flying airplane), so say its a small ventilator standing on my desk. What I want to know is the volume flow of air its generating at a certain motor rpm. This is what I do:

Prop pitch = 6"
Prop dia. = 9"
Motor rpm = 2000rpm

For 1 rotation, the prop moves the air 6"
For 2000 rotations, this means 12000". So the theoretical airflow speed would be 1000ft/min.
The disk area works out to 0,44 square foot.
So this would mean a volume flow of 440 CFM

Now my question; in how far is this value representative for the real flow? Does there exist a coefficient which takes this into account?
If someone could tell me a rough value this would also be good for giving me an idea..
 
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  • #2
Good question, I assume that if the propeller is standing mounted on your desk that more power is consumed (for equal amount of thrust) to feed or draw in the air.

Perhaps there is a "ram air" factor which must be added, or a feed air equation which must be subtracted.

If you get your question answered, maybe I can get a related answer for A, B & C.
 

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  • #3


Thanks for the question!

Theoretical airflow speed of a rotating propeller is a good starting point, but it is important to keep in mind that there are many factors that can affect the actual airflow speed. In a real-life scenario, the propeller will encounter air resistance, turbulence, and other external factors that can impact its performance. Therefore, it is difficult to give a precise value for the realistic airflow speed.

One way to estimate the realistic airflow speed is by using a propeller efficiency coefficient. This coefficient takes into account the propeller design, blade shape, and other factors to give a more accurate representation of the actual airflow speed. The efficiency coefficient typically ranges from 0.7 to 0.9, with higher values indicating a more efficient propeller.

In your example, with a theoretical airflow speed of 1000ft/min and a disk area of 0.44 square foot, using an efficiency coefficient of 0.8, the realistic airflow speed would be around 800ft/min. This would result in a volume flow of approximately 352 CFM. Keep in mind that this is just an estimate and the actual airflow speed may vary depending on the specific propeller and motor setup.

I hope this helps clarify the concept of theoretical airflow speed and how it relates to realistic values. It is always important to consider other factors and use coefficients to get a more accurate representation of the actual airflow speed in real-life scenarios.
 

Related to From theoretical airflow speed of rotating propeller to a realistic value?

1. What is the purpose of studying the theoretical airflow speed of a rotating propeller?

Theoretical airflow speed of a rotating propeller is important in understanding the performance and efficiency of a propeller. It helps in determining the maximum potential speed that the propeller can achieve and also aids in the design process.

2. How is the theoretical airflow speed of a propeller calculated?

The theoretical airflow speed of a rotating propeller can be calculated using the propeller's diameter, pitch, and rotational speed. This calculation is based on the assumption of an ideal fluid flow and does not take into account factors such as air density and drag.

3. Is the theoretical airflow speed of a propeller the same as its actual speed?

No, the theoretical airflow speed is an ideal value and does not account for real-world factors such as air density and drag. Therefore, the actual speed of a propeller will be lower than its theoretical speed.

4. How does the angle of attack affect the theoretical airflow speed of a rotating propeller?

The angle of attack, which is the angle between the propeller blade and the direction of the oncoming airflow, can affect the theoretical airflow speed. A higher angle of attack can lead to a higher theoretical speed, but it can also cause drag and reduce the propeller's efficiency.

5. Can the theoretical airflow speed of a propeller be measured in real-world conditions?

No, the theoretical airflow speed is a calculated value and cannot be directly measured in real-world conditions. However, it can be used as a baseline for comparison with the actual speed of a propeller in different operating conditions.

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