Stream thrust averaging

In fluid dynamics, stream thrust averaging is a process used to convert three-dimensional flow through a duct into one-dimensional uniform flow. It makes the assumptions that the flow is mixed adiabatically and without friction. However, due to the mixing process, there is a net increase in the entropy of the system. Although there is an increase in entropy, the stream thrust averaged values are more representative of the flow than a simple average as a simple average would violate the second Law of Thermodynamics.

Equations for a perfect gas

Stream thrust:

$F = \int \left(\rho \mathbf{V} \cdot d \mathbf{A} \right) \mathbf{V} \cdot \mathbf{f} +\int pd \mathbf{A} \cdot \mathbf{f}.$

Mass flow:

$\dot m = \int \rho \mathbf{V} \cdot d \mathbf{A}.$

Stagnation enthalpy:

$H = {1 \over \dot m} \int \left({\rho \mathbf{V} \cdot d \mathbf{A}} \right) \left( h+ {|\mathbf{V}|^2 \over 2} \right),$

$\overline{U}^2 \left({1- {R \over 2C_p}}\right) -\overline{U}{F\over \dot m} +{HR \over C_p}=0.$

Solutions

Solving for $\overline{U}$ yields two solutions. They must both be analyzed to determine which is the physical solution. One will usually be a subsonic root and the other a supersonic root. If it is not clear which value of velocity is correct, the second law of thermodynamics may be applied.

$\overline{\rho} = {\dot m \over \overline{U}A},$

$\overline{p} = {F \over A} -{\overline{\rho} \overline{U}^2},$

$\overline{h} = {\overline{p} C_p \over \overline{\rho} R}.$

Second law of thermodynamics:

$\nabla s = C_p \ln({\overline{T}\over T_1}) +R \ln({\overline{p} \over p_1}).$

The values $T_1$ and $p_1$ are unknown and may be dropped from the formulation. The value of entropy is not necessary, only that the value is positive.

$\nabla s = C_p \ln(\overline{T}) +R \ln(\overline{p}).$

One possible unreal solution for the stream thrust averaged velocity yields a negative entropy. Another method of determining the proper solution is to take a simple average of the velocity and determining which value is closer to the stream thrust averaged velocity.

References

• DeBonis, J.R.; Trefny, C.J.; Steffen, Jr., C.J. (1999). "Inlet Development for a Rocket Based Combined Cycle, Single Stage to Orbit Vehicle Using Computational Fluid Dynamics" (PDF). NASA/TM—1999-209279. NASA. Retrieved 18 February 2013.