Alternative form of Reynold's number

In summary, the conversation discusses the relationship between π1 and π2, where π1 is the inverse of the Reynolds number. The main question is whether it is correct to express π1 as a function of π2 or if it should be written as the Reynolds number itself. It is clarified that double prime (") indicates the second derivative of a function. The answer is that both ways of expressing π1 are correct, but in aeronautics, it is more common to write it as the inverse of the Reynolds number. The conversation also mentions that π1 and π3 are related in some way to π2, but it is not specified how.
  • #1
foo9008
678
4

Homework Statement


in the third picture , we know that π2 can be written as function of π1 , where π2 is inverse of reynold number , how if i want to change it to π1 = function of π2 , can i write it as (Reynold number ) = F / ρ (D^2)(v^2) ?

p/s : π1 is actually inverse of reynold number

Homework Equations

The Attempt at a Solution


IMO , for π1 = function of π2 , it is also (Reynold number ) = f (F / ρ (D^2)(v^2) ) ... we should write it as reynold number instead of inverse of reynold number , am i right ?
 

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  • #2
What does upper case phi double prime stand for?

Φ'' (Re) = FD/ρD2V2
 
  • #3
David Lewis said:
What does upper case phi double prime stand for?

Φ'' (Re) = FD/ρD2V2
I think the author means stand for function...
 
  • #4
David Lewis said:
What does upper case phi double prime stand for?

Φ'' (Re) = FD/ρD2V2
do u have any idea now ?
 
  • #5
anyone know the answer?
 
  • #6
OK. If Φ represents a function then double prime would normally indicate the second derivative of that function.
 
  • #7
David Lewis said:
OK. If Φ represents a function then double prime would normally indicate the second derivative of that function.
can i write it as (Reynold number ) = F / ρ (D^2)(v^2) ?

or , it should be 1/ reynold number = F / ρ (D^2)(v^2) ?
which one is correct ?
 
  • #8
1/Re = F/ρD2V2

where F = viscous forces
 
  • #9
David Lewis said:
1/Re = F/ρD2V2

where F = viscous forces
is it wrong to write it as (Reynold number ) = F / ρ (D^2)(v^2) ?
is there a need to change 1/ Re to Re for π1 in this case
P/s : π1 = function of ( π2 , π3 )
 
  • #10
The Reynolds number is dimensionless, so the numerator and denominator will have the same fundamental dimensions (M, L, T).

In aeronautics, the denominator (viscous forces) is smaller than the numerator (inertial forces) -- possibly 5 or 6 orders of magnitude smaller -- which makes Re a large number.
 
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  • #11
David Lewis said:
The Reynolds number is dimensionless, so the numerator and denominator will have the same fundamental dimensions (M, L, T).

In aeronautics, the denominator (viscous forces) is smaller than the numerator (inertial forces) -- possibly 5 or 6 orders of magnitude smaller -- which makes Re a large number.
So, no matter pi 1 is Reynold number = ( pi 2 , pi3) or pi 1 is 1/ reynold number d= ( pi2, pi3) are correct??
 
  • #12
2 = FD/ρD2V2

What do ∏1 and ∏3 equal?
 

Related to Alternative form of Reynold's number

1. What is the alternative form of Reynold's number?

The alternative form of Reynold's number is known as the Strouhal-Reynolds number and is represented by the equation Re* = U/ν*L, where U is the characteristic velocity, ν is the kinematic viscosity, and L is the characteristic length.

2. How is the Strouhal-Reynolds number different from the traditional Reynold's number?

The Strouhal-Reynolds number incorporates the Strouhal number, which measures the ratio of unsteady inertial forces to viscous forces, into the traditional Reynold's number equation. This accounts for the effects of flow unsteadiness on the flow behavior.

3. When is the Strouhal-Reynolds number used instead of the traditional Reynold's number?

The Strouhal-Reynolds number is typically used in situations where the flow is unsteady, such as in pulsatile flow or vortex shedding, as it provides a more accurate representation of the flow behavior. It is also commonly used in aerodynamics and hydrodynamics research.

4. How do you calculate the Strouhal-Reynolds number?

To calculate the Strouhal-Reynolds number, you need to know the characteristic velocity, kinematic viscosity, and characteristic length of the flow. Once these values are known, simply plug them into the equation Re* = U/ν*L to determine the Strouhal-Reynolds number.

5. What are the applications of the Strouhal-Reynolds number?

The Strouhal-Reynolds number is used in a variety of fields, including aerodynamics, hydrodynamics, and fluid mechanics. It is particularly useful in studying unsteady flows and can help predict the occurrence of vortex shedding and other flow instabilities. It is also used in the design and analysis of various engineering systems, such as turbines and propellers.

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