Fundamentals of Fluid Mechanics Questions and Answers
 Question by AME536A Student For homework #12 question #2, are we able to solve for lift and drag on the different sections of the air foil and sum them together? In addition, should the question include the value for L?
 12.08.19
Question #2 is clear, just answer the question.
 Question by AME536A Student On assignment #12 on question #4, the answer given is for the drag coefficient right? If that's the case, I think that there is a mistake there and it should be $C_d=\frac{4m^2}{(2m-1)\sqrt{M_\infty^2-1}} \left( \frac{h}{t}\right)^2\frac{1}{\sqrt{\left( \frac{h}{t}\right)^2+1}}$.
 $\pi$