Total energy of air, does it include pressure?

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SUMMARY

The discussion centers on the total energy of air in relation to pressure and drag forces experienced by a bus in motion. It establishes that the work done on the air is influenced by both the kinetic energy change and the pressure energy of the air. The example of two buses, one with a streamlined tail section, illustrates the relationship between drag forces and speeds, emphasizing that the drag force is a combination of pressure drag and shear frictional drag. The integral sum of kinetic energy calculations for both buses raises questions about the influence of immediate velocities versus exit velocities on work done.

PREREQUISITES
  • Understanding of aerodynamic drag forces
  • Familiarity with kinetic energy equations
  • Knowledge of pressure differentials in fluid dynamics
  • Basic principles of mass flow and velocity in airflow
NEXT STEPS
  • Research the principles of aerodynamic drag and its components, including pressure drag and shear frictional drag.
  • Study the equations governing kinetic energy, particularly in the context of fluid dynamics.
  • Explore the concept of pressure energy in relation to moving fluids and its impact on work done.
  • Investigate the effects of streamlined designs on drag reduction in vehicles.
USEFUL FOR

Aerospace engineers, mechanical engineers, and anyone involved in vehicle design and optimization, particularly in understanding aerodynamic efficiency and drag forces.

rcgldr
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I'll ask this in the form of an example. A bus is traveling at some speed and there is no wind. The bus experiences a drag force related to the pressure differential at the front and rear of the bus. Most of the divergence in pressure from ambient occurs behind the bus, where the air is accelerated forward to fill in what would otherwise be a void.

The power consumption related to drag should be this drag force times speed (this is a no wind condition, so ground speed = air speed).

The "exit velocity" for each tiny amount of mass of air affected by the bus it that bit of air's velocity at the moment and place where it's pressure returns to ambient. Will the work done on the air by the bus be equal to the integral sum of 1/2 mass (exit_velocity)2?

The velocities in the immediate vicinity of the bus will be different than the exit velocities. The higher pressure areas will have velocities lower than exit velocity and vice versa. Is the work done on the air instead related to these velocities as opposed to the exit velocities?

Now to reask the original question, is the work done only related to the kinetic energy change of the air, or is the pressure energy of the air also a factor?

another example

Take a second bus with a streamlined tail section to reduce the drag. Bus2 travels faster so that it consumes the same amount of aerodynamic power as bus1 :

drag2 speed2 = drag1 speed1

Will the integral sum of the 1/2 mass (immediate_velocites)2 or 1/2 mass (exit_velocities)2 (or maybe both?) be the same for bus1 and bus2?
 
Last edited:
Physics news on Phys.org
The air drag on an object is a combination of pressure drag (component of force normal to surface of object) and shear frictional drag (component of force tangent to surface of object).
 

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