How Fast Must Wind Blow to Lift an Aluminum Sheet?

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SUMMARY

The discussion focuses on calculating the minimum wind velocity required to lift a 0.01 m thick aluminum sheet using principles from fluid dynamics. The density of air is given as 1.18 kg/m³ and aluminum as 2700 kg/m³. Participants suggest using Bernoulli's Equation and the concept of pressure differences, similar to lift on an airplane wing, to determine the necessary conditions for the sheet to rise. The key steps involve calculating the weight per area of the aluminum sheet and the corresponding pressure difference needed to initiate lift.

PREREQUISITES
  • Understanding of Bernoulli's Equation
  • Familiarity with Archimedes' Principle
  • Basic knowledge of fluid dynamics
  • Ability to calculate pressure and density
NEXT STEPS
  • Study Bernoulli's Equation in detail to understand pressure differences
  • Learn about lift generation in aerodynamics, particularly for airfoils
  • Explore buoyancy and Archimedes' Principle in various fluids
  • Investigate the relationship between wind speed and pressure changes over surfaces
USEFUL FOR

Students in physics or engineering, particularly those studying fluid dynamics, aerodynamics, or materials science, will benefit from this discussion.

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Homework Statement



A sheet of aluminum of thickness .01 m lies in a parking lot. A wind blows over the top of the sheet. What is the minimum velocity that will cause the sheet to begin to rise: Assume the density of air is 1.18 kg/m^3 and aluminum is 2700 kg/m^3.

Homework Equations



Bernoulli's Equation:

82cf4ee7e0214e063ea7d24787380f8a.png


or

Archimedes Principal:

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Density = M/Vol

The Attempt at a Solution



I really have no idea where to start. Since the density of AL is different than that of the fluid, I would assume it to be a buoyant force. However, air is a strange fluid to work with, and I can't figure out the volume displaced.

I just need a hint on where to begin... maybe some links to other reading. All help would be vastly appreciated.

Thanks! Sean
 
Last edited by a moderator:
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well its much like the lift on a wing where the difference in velocities leads to a pressure gradient across the sheet.
 
First figure out the weight per area of the aluminum sheet in N/m^2, based the numbers given. That weight per area is then the difference in pressure needed to lift the plate. Assume the air below the plate is still, and figure out how fast the air on top of it needs to be to create the pressure difference.
 

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