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". NASA/TM—1999-209279. NASA. http://gltrs.grc.nasa.gov/reports/1999/TM-1999-209279.pdf. Retrieved 2011-02-09.
