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We assume static pressure of a fluid coming out of a pipe or nozzle of gas turbine with high temperature and velocity is equal to atmospheric pressure, which confuses me for some point.

Does it mean that a fluid in atmosphere can not have more or less static pressure than atmospheric pressure?

For instance,

There is stationary air in room. It has no kinetic energy, so no dynamic pressure. It has only static pressure which is equal to atmospheric pressure.

Now, we suddenly add kinetic energy to it by turning a big fan on.

Its previous condition: enter link description here

Its current condition: enter link description here

Is static pressure in condition 2 equal to Patm or less than Patm?

I think total pressure in condition 1 and 2 can't be equal to each other, since we add extra energy. So, static pressure in condition 2 should be still equal to Patm.

When this fluid comes to a rest by hitting the wall, its static pressure will be its total pressure and be more than Patm.

Do you agree?

Fred
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Jawel7
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3 Answers3

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You are forgeting a very important law and a very important equation, namely the Bernoulli equation. The Bernoulli equation is essentially an equation of conservation of energy. It goes:

$p_{s} + p_{d} + p_{h} = C$

meaning that the static pressure, the dinamic pressure and the hydrostatic pressure (which we will not take in consideration here) have to be constant, C is just some constant number. You can look at this like a pendulum that exchanges its potential and kinetic energy with each swing, but the constant energy in the system remains constant.

So when you bring more kinetic energy in the system (in your case that is the dinamic pressure) the static pressure must diminish. Thus in your case the $P_{t2}$ the static pressure will be have to decrease and be lower than the atmospheric pressure!

Here is a link to the Bernoulli equation on the Wiki. An very important equation, a form of conservation of energy for fluids.

https://en.wikipedia.org/wiki/Bernoulli%27s_principle

User198
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The Bernoulli equation applies to conservative flow, meaning there is no added head or energy midstream. If there is a source or sink midway, it has to be accounted for.

You are right. If you add energy by placing a fan in the stream, the pressure is the sum of static and dynamic pressure. The same thing happens in a turbocharged carborator, a jet engine, and so on. The reverse of this is also true. The static pressure of air drops after passing through a windmill.

Here is the Wikipedia image of an axial fan flow diagram.

  • C is speed
  • P pressure

'

wiki

kamran
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Of course it can, this is the nature of airfoils. Furthermore, atmospheric pressure changes across the world - a barometer is used to measure this. The result of different atmospheric pressures? Wind.

In general, "the atmosphere" is treated like a plenum, which is generally defined as a place where everything has the same pressure. But as you dig in its easy to find exceptions.

Tiger Guy
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