What are aerodynamics benefits of using un loadedunloaded wingtips (zero lift),does? does unloaded wingtip make inner parts of wing works more effecientefficient?
(I know that un loadunloaded wingtip reducereduces bending moment,so structural weight can be lower,thus thus reduction in L/D and higher net wing lift (lift minus wing weight), but you can conectconnect wingtip with wire and use elipticalelliptical distribution..so..)
What are aerodynamics benefits of using un loaded wingtips(zero lift),does unloaded wingtip make inner parts of wing works more effecient?
(I know that un load wingtip reduce bending moment,so structural weight can be lower,thus reduction in L/D and higher net wing lift(lift minus wing weight), but you can conect wingtip with wire and use eliptical distribution..so..)
What are aerodynamics benefits of using unloaded wingtips (zero lift)? does unloaded wingtip make inner parts of wing more efficient?
(I know that unloaded wingtip reduces bending moment,so structural weight can be lower, thus reduction in L/D and higher net wing lift (lift minus wing weight), but you can connect wingtip with wire and use elliptical distribution..so..)
What are aerodynamics benefits of using un loaded wingtips(zero lift),does unloaded wingtip make inner parts of wing works more effecient?
(I know that un load wingtip reduce bending moment,so structural weight can be lower,thus reduction in L/D and higher net wing lift(lift minus wing weight), but you can conect wingtip with wire and use eliptical distribution..so..)
What are aerodynamics benefits of using un loaded wingtips(zero lift),does unloaded wingtip make inner parts of wing works more effecient?
(I know that un load wingtip reduce bending moment,so structural weight can be lower,thus reduction in L/D, but you can conect wingtip with wire and use eliptical distribution..so..)
What are aerodynamics benefits of using un loaded wingtips(zero lift),does unloaded wingtip make inner parts of wing works more effecient?
(I know that un load wingtip reduce bending moment,so structural weight can be lower,thus reduction in L/D and higher net wing lift(lift minus wing weight), but you can conect wingtip with wire and use eliptical distribution..so..)
