What creates a partial vacuum when a fan is in motion?

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    Fan Partial Vacuum
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Discussion Overview

The discussion centers on the physical mechanisms behind the creation of a partial vacuum when a fan is in motion. Participants explore the implications of airflow dynamics, pressure changes, and the behavior of air molecules in relation to the fan blades.

Discussion Character

  • Exploratory
  • Technical explanation
  • Conceptual clarification

Main Points Raised

  • One participant suggests that a spinning fan creates a partial vacuum by pushing air molecules away, resulting in lower pressure in the vicinity of the fan.
  • Another participant agrees, indicating that the motion of the blades leads to regions of varying air molecule density, which may affect the velocity field of the air.
  • A further contribution discusses the pressure dynamics, explaining that the reduced pressure on the intake side is due to the fan blades receding from the air, creating a pressure gradient that accelerates incoming air.
  • This participant also mentions that after air crosses the fan blades, there is a pressure jump, but the speed does not change significantly, with an approximation provided for the air speed as it exits the fan.
  • A link to a NASA article is shared to illustrate a similar effect observed in propellers, noting simplifications in the airflow model presented.

Areas of Agreement / Disagreement

Participants generally agree on the basic mechanism of how a fan creates a partial vacuum and the role of pressure gradients, but the discussion includes varying levels of detail and complexity regarding airflow dynamics and pressure changes.

Contextual Notes

Some assumptions about airflow behavior and pressure dynamics remain unaddressed, and the discussion does not resolve the complexities of variable density fields in relation to the momentum equation for air particles.

Who May Find This Useful

This discussion may be of interest to individuals studying fluid dynamics, engineering principles related to airflow, or those curious about the physics of fans and propellers.

Sarcina
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My understanding is that when a fan begins spinning, a partial vacuum is created. Physically, what creates this partial vacuum? Does the motion of the blades create a void in which there are fewer air molecules than in the ambient air and thus the pressure is lower than the ambient pressure?
 
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Essentially, yes. The blades of the fan physically push molecules of air out of the way, leaving a partial vacuum behind until more air can move into replace them.
 
Thank you. So a spinning fan creates regions where there are less air molecules than ambient air as well as regions where there are more air molecules than ambient air; I guess this will change the density of the macroscopic air particles near the fan? Does this mean that to determine the velocity field for the macroscopic air particles near a spinning fan, you would need to solve the momentum equation for air particles with a variable density field?
 
The reduced pressure on the intake side of a fan is due to the intake side surfaces of the fan blade receding away from the air. What would be a void left behind by the fan blade is filled in by air accelerating towards the fan blade, but since the air has momentum, it takes a force to produce the acceleration, and the force is due to a pressure gradient where pressure decreases as the air approaches the intake side of a fan. Once the air crosses the fan. there's a jump in pressure, but not much change in speed. The increased pressure causes the air to continue to accelerate, and after the jump in pressure, the pressure decreases with distance from the output side of the fan. An approximation for the speed of the air as it crosses the fan blades is about 1/2 of the air's "exit" speed, which is the speed of the air as it's pressure returns to ambient.

Here is a link to a Nasa article about propeller's showing a similar effect. Note that the decreasing cross section of the affected air in that article is simplified, ignoring the effects of vicosity at the outer edges of the idealized air flow.

http://www.grc.nasa.gov/WWW/K-12/airplane/propanl.html
 
Thank you very much.
 

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