consider two different wings designed with different airfoil shapes. both have rectangular planforms but wing 1 has a chord of 1m and a span of 16m while wing2 has a chord of 2m and a span of 15m. assume the flight speed is 55.88m/s and the air density is 1.112kg/m3. at this flight condition, wing1 generates 41667n of lift force, while wing 2 generates 50284n of lift. which wing do you think is more efficient? why? hint: think of how well each wing makes use of the available dynamic pressure to produce lift.
