Calculate the average circulation of wing span b=5 meters which generates L=2489 N of lift and flies at V=66 m/s in air
Posted: Tue Jun 07, 2022 2:14 pm
Calculate the average circulation of wing span b=5 meters which generates L=2489 N of lift and flies at V=66 m/s in air of density 0.8 kg/m3. Circulation is measured in (m2/s). Answer: