Compressible Flow Scores
 2017
 08.31.17
 2018
 09.05.18
The grades for Assign 0 have been entered. I gave A0 if you registered but didn't enable email notifications in the Compressible Flow forum, and “-” if you didn't register.
 09.07.18
Quiz 1 has been corrected. I gave A0 if you didn't explain well enough all the steps to reach an answer.
 09.28.18
Quiz 2 has been corrected. You all did fine.
 10.12.18
Quiz 3 has been corrected. I took away half a grade if you didn't write all the steps in finding $\gamma$. You can't just say it was found the calculator from a complex expression. You need to isolate $\gamma$ and then calculate it.
 10.19.18
Note that a grade for Assign 4 will be given after the Quiz on Tuesday. This Tuesday (Oct 30), the quiz question will be either from Assignment 4 or from Design 1. Make sure you can remember your solutions.
 10.27.18
The grades for A4/D1 are inputted. I took away a half grade if you didn't finish the problem fully or made an important mistake.
 11.01.18
Quiz 7 is corrected: I gave you all A0. Although you didn't all do it the same way, you all made a mistake in how you setup your integral. You shouldn't have to say $\cos(\theta)=1$ because $\theta$ is small. This is not needed here and shouldn't be done. What you need to think more about is how to setup the integral. Hint: the total lift force per unit span is $F_{\rm L}=\int_{x=0}^{x=t} (P_{\rm bottom}-P_{\rm top}) dx$.
 $\pi$