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Fluid flow limit for given orifice Question
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Posted by: SJB ®

08/12/2005, 07:16:35

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I recall from fluid flow studies during my A level Engineering Science course (over twenty years ago, ahem) that any orifice has a throttle point beyond which no matter how much additional pressure is supplied, a given fluid cannot flow any greater volume.

Because I can't remember the name of this phenomenon, and don't currently have my course books and written notes to hand, please will you be kind enough to point me in the direction of where I can refresh my memory.

The subject has arisen with respect to turbocharger boost pressure on petrol engines; in other words the point at which all you are going to get is additional heat. A lot of it.


Many thanks!







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Re: Fluid flow limit for given orifice
Re: Fluid flow limit for given orifice -- SJB Post Reply Top of thread Forum
Posted by: Raph0007 ®

08/12/2005, 16:07:34

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I think you are looking for "choking". Although it has been a long time since I studied this myself..

A good refresher course can be found at the NASA site:

https://www.grc.nasa.gov/WWW/K-12/airplane/mflchk.html

look for equation #19

Hope this helps

Raph







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Re: Re: Fluid flow limit for given orifice
Re: Re: Fluid flow limit for given orifice -- Raph0007 Post Reply Top of thread Forum
Posted by: mbeychok ®

09/15/2005, 01:37:48

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Raph0007:

The velocity of gas flowing through an orifice becomes choked (and is also referred to as sonic velocity) when the ratio of the absolute upstream pressure to the absolute downstream pressure is equal to or greater than [ ( k + 1 ) / 2 ] k / ( k - 1 ), where k is the specific heat ratio of the discharged gas.  For many gases, k ranges from about 1.09 to about 1.41, and thus [ ( k + 1 ) / 2 ] k / ( k - 1 ) ranges from 1.7 to about 1.9 ... which means that choked velocity usually occurs when the absolute upstream pressure is at least 1.7 to 1.9 times as high as the absolute downstream pressure.

In the customary units used in the USA, when the gas velocity is choked, the equation for the mass flow rate is:

Q = C A [g k d P]1/2[2/(k+1)](k+1)/(2k-2)

or this equivalent form:

Q = C A P[g k M/(R T)]1/2[2/(k+1)](k+1)/(2k-2)

It is important to note that although the gas velocity reaches a maximum and becomes choked, the mass flow rate is not choked. The mass flow rate can still be increased if the source pressure is increased.

Q = mass flow rate, lb/s
C = discharge coefficient (dimensionless, usually about 0.72)
A = discharge hole area, ft2
g = gravitational acceleration of 32.17 ft/s2
k = gas cp/cv = (specific heat at constant pressure)/(specific heat at constant volume)
d = gas density, lb/ft3, at upstream pressure
P = absolute upstream pressure, lb/ft2
M = gas molecular weight
R = the Universal Gas Law Constant = 1545.3 (ft-lb)/(lbmol)(°R )
T = gas temperature, °R

Milton Beychok






Modified by mbeychok at Fri, Sep 16, 2005, 12:20:09

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Re: Fluid flow limit for given orifice
Re: Re: Fluid flow limit for given orifice -- Raph0007 Post Reply Top of thread Forum
Posted by: SJB ®

08/12/2005, 19:19:39

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Many thanks, Raph.

Most useful, and the information contained in your link lead to further information that was similarly so.

Choking was indeed the subject.







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