HOMEWORK #5

 
Part A:    Due Friday Mar 22
Parts B&C: Due Wednesday Mar 27

1. plots of
   1. Cp vs x/c for alpha = -2, 0, 2,4
   2. Cp vs y/c for alpha = -2, 0, 2,4
2. table of
   1. Cx vs alpha
   2. Cz vs alpha
   3. Cl vs alpha
   4. Cd vs alpha
3. plots of
   1. Cl vs alpha
   2. Cd vs alpha
   3. Cd vd Cl

Submit only:
1. Spread sheets
   1. Showing values
   2. Showing equations
2. Copies of all required graphs
3. Plot of airfoil shape

Note:

TAP#1 Ignore
TAP#2 measures test section pressure (relative to itself)
TAP#22 measures settling chamber pressure (relative to the test section pressure). Assume it is equal to stagnation pressure.
All the others correspond to the locations indicated