Re: Aerodynamic modifications
About the 787 wingtips, doubt they studied birds for the design. They were driven by; reduced wing root bending moment provided by the reduced wing area out at the tip due to the narrow tip chord, reduced induced drag since airliners cruise at moderate CL's of 0.5 or so, and getting the shock to sweep at the tips to minimize wave drag. The first two are factors in bird evolution. The sweep also reduces profile drag in the subsonic, 'bird', domain. Those guys are pretty sharp though to figure all of that out.
You can do the same thing with winglets. Reducing the winglet tip chord to a minimum reduces the structural weight required to hang onto them.
About the 787 wingtips, doubt they studied birds for the design. They were driven by; reduced wing root bending moment provided by the reduced wing area out at the tip due to the narrow tip chord, reduced induced drag since airliners cruise at moderate CL's of 0.5 or so, and getting the shock to sweep at the tips to minimize wave drag. The first two are factors in bird evolution. The sweep also reduces profile drag in the subsonic, 'bird', domain. Those guys are pretty sharp though to figure all of that out.
You can do the same thing with winglets. Reducing the winglet tip chord to a minimum reduces the structural weight required to hang onto them.
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