Stream thrust averaging

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