Use CFR approach covered in class. For the gust lines, assume an altitude density of rho=0.00200 slug/ft³. From each V-N diagram, determine the max/min load factors for wing design.

a) Max Load Factor: 0.00200/ft³, Min Load Factor: 0.00200/ft³
b) Max Load Factor: 0.00200, Min Load Factor: 0.00400
c) Max Load Factor: 0.00400, Min Load Factor: 0.00200
d) Max Load Factor: 0.00400/ft³, Min Load Factor: 0.00400/ft³