Relation Between Ma and Re for Isentropic Expansion

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Homework Help Overview

The problem involves investigating the relationship between the Reynolds number (Re) and the Mach number (M) during the isentropic expansion of air from a fixed reservoir. The original poster attempts to show that Re decreases for increasing M, particularly for M much greater than 1, while considering the temperature dependence of viscosity using the Power Law.

Discussion Character

  • Exploratory, Assumption checking

Approaches and Questions Raised

  • Participants discuss the original poster's approach to calculating Re using the Power Law for viscosity and the isentropic expansion equations. Questions arise regarding the geometry of the flow, with some participants seeking clarification on whether the flow occurs through a pipe with varying diameter.

Discussion Status

The discussion is ongoing, with participants exploring the implications of the lack of provided geometry and its relevance to the problem. There is a focus on the specific use of the Power Law for viscosity, and some guidance is offered regarding the assumption of flow through a pipe.

Contextual Notes

Participants note that the problem does not specify geometry, which may affect the interpretation of the flow conditions. The original poster's observations about the behavior of Re in relation to M are also under scrutiny.

Ankith
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Homework Statement


Consider the isentropic expansion of air from a fixed given reservoir (i.e. total pressure and temperature). Investigate the behaviour of the value of the Reynolds number of the flow, as a function of the Mach Number M of the expanded flow.
For small values of M, the thermodynamic properties of the flow will not deviate signifciantlz from the reservoir conditions, hence Re increases linearly with U and therefore with M.

How do I show that for increasing expansion (i.e. increasing M) the value fo Re will eventually decrease, by investigating the limit behaviour for M>>1. I must emplease the temperature dependence of viscosity using the Power Law.
Sutherlands Constant, S=111 K

Homework Equations


Power Law: mu/mu_0=[(T/T_0)][w] , where w=3/2 - T_0/T_0+S

The Attempt at a Solution


T_0=288K
w=0.778
Substituting in Power Law,
mu=1.81*10^(-5)*(T/288)^0.778

Now Re=rho*U*L/mu

Re=rho*sqrt(R*gamma*T_0*M)/mu

For different values of M, I can calculate T using the isentropic expansion equation, subsititute that value of T in the equation to calculate mu, and further substitute the Mach number and value of 'mu' in the Reynolds number equation. This can thus give me the distribution of the Reynolds number for different Mach numbers.

However, after plotting what I observe is that the Re continues to linearly increase, which is not what the question states, as I must observe a reduction in the value of Re after Ma=1.
 
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What exactly it the geometry? Can you please provide a sketch?
 
There is no geometry provided. The question is very specific to using the power law for the temperature dependence of viscosity. Which is why an area ratio is not really meant to be considered.
 
Chestermiller said:
What exactly it the geometry? Can you please provide a sketch?
2 / 0

There is no geometry provided. The question is very specific to using the power law for the temperature dependence of viscosity. Which is why an area ratio is not really meant to be considered.
 
Ankith said:
There is no geometry provided. The question is very specific to using the power law for the temperature dependence of viscosity. Which is why an area ratio is not really meant to be considered.
So you have air flow through a pipe of increasing cross sectional diameter?
 
Chestermiller said:
So you have air flow through a pipe of increasing cross sectional diameter?
I believe that would be our best bet. That is what I have assumed as well.
 

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