Wing A has a constant chord c and span b. Wing B is identical but has a span 4b. When both wings are operating at the same geometric angle of attack at subsonic speed, then:

wing A produces a smaller lift coefficient than wing B

wings A and B produce the same lift coefficient

wing A produces a greater lift coefficient than wing B

the freestream Mach number decides which wing produces the greater lift coefficient

Wing A has a constant chord c and span b. Wing B is identical but has

1.	Wing A has a constant chord c and span b. Wing B is identical but has a span 4b. When both wings are operating at the same geometric angle of attack at subsonic speed, then:
A.	wings A and B produce the same lift coefficient
B.	wing A produces a smaller lift coefficient than wing B
C.	wing A produces a greater lift coefficient than wing B
D.	the freestream Mach number decides which wing produces the greater lift coefficient
Answer» B. wing A produces a smaller lift coefficient than wing B