Computational Aerodynamics Scores  






Quiz #1 has been corrected.


Quiz #2 has been corrected.


Quiz #4 has been corrected. You got A+ if there was no major logical flaw in your reasoning. I gave A0 to those who made at least one major mistake such as saying that $P=P(T)$. Of course, this is incorrect because $P=P(\rho_1,\rho_2,T)$.


Quiz #5 has been corrected. I took away half a grade if you couldn't get the right perpendicular Mach number to the exit area.


Quiz #6 has been corrected. I gave you B+ if you couldn't find $u_{i+1/2}^{(4)}$ from the answers. If you understood part (d) correctly, you should know how to do this.


Quiz #7 has been corrected. I gave A0 if you didn't compute the answer using fractions. I also gave A0 if you didn't indicate clearly how you found $A$ at the interface. Note that $A(u_{\rm L},~u_{\rm R})$ should be first written as $A(u_{i+1/2})$ and then evaluated. If you skipped that step, you were given A0.


The final exams have been corrected.


The final grades have been adjusted.



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