MolaKule
Staff member
I don't think this topic has been discussed before but this is an interesting concept.
https://simpleflying.com/nasa-boeing-sustainable-flight-demonstrator-project/
They will be taking a DC-90 fuselage and moving the wings to the top of the fuselage with underwing mounted engines.
Since the wings will be long and thin 'glider-type' wings, a strut will support the wing.
Due to the length of the wings, they will have to be segmented fold-up types in order to dock at conventional gates.
I haven't seen any X-66 wing profiles in the public domain but I suspect it will be a modified version of the NACA 661212-il profile or something similar.
One thing for sure, lift is a very strong function of the airfoil camber:
https://en.wikipedia.org/wiki/Camber_(aerodynamics)
FWIW, here's how we learned to analyze wings at Embry-Riddle:
https://eaglepubs.erau.edu/introduc...icles/chapter/worked-examples-airfoils-wings/
https://simpleflying.com/nasa-boeing-sustainable-flight-demonstrator-project/
They will be taking a DC-90 fuselage and moving the wings to the top of the fuselage with underwing mounted engines.
Since the wings will be long and thin 'glider-type' wings, a strut will support the wing.
Due to the length of the wings, they will have to be segmented fold-up types in order to dock at conventional gates.
I haven't seen any X-66 wing profiles in the public domain but I suspect it will be a modified version of the NACA 661212-il profile or something similar.
One thing for sure, lift is a very strong function of the airfoil camber:
https://en.wikipedia.org/wiki/Camber_(aerodynamics)
FWIW, here's how we learned to analyze wings at Embry-Riddle:
https://eaglepubs.erau.edu/introduc...icles/chapter/worked-examples-airfoils-wings/
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