The main difference between the CL curves for straightwing aircraft is that a. the sweptwing aircraft has

The main difference between the CL–α curves for straight‐wing aircraft is that

a. the swept‐wing aircraft has a lower value of CL(max).

b. the straight‐wing aircraft does not fly at as high an AOA for CL(max).

c. the swept‐wing aircraft does not have an abrupt loss of lift at CL(max).

d. All of the above.