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- W1489211523 abstract "Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by appropriate design of fuselage and roots. Abrupt changes from maximum fuselage height to chord must be avoided and every longitudinal section of fuselage and roots must be so faired and arranged as to preserve the original lift distribution of the continuous wing. Adapting the fuselage to the curvilinear circulation of the affords further improvement. The polars of such arrangements are almost the same as those of the wing alone, thus voiding the superiority of the high-wing type airplane known with conventional design." @default.
- W1489211523 created "2016-06-24" @default.
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- W1489211523 date "1935-02-01" @default.
- W1489211523 modified "2023-09-27" @default.
- W1489211523 title "The aerodynamic aspect of wing-fuselage fillets" @default.
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