The paper will deal with the design of the aircraft, starting from a market survey, conceptual design loop and preliminary choice of dimensions up to detailed design of an efficient high-lift systems and low-drag fuselage shape. Technological challenges regarding the design of low-cost systems for the flap/slat retraction and simple wing folding system will be highlighted. Aiming to an efficient optimization algorithm, it has been developed a new integration technique between CAD, aerodynamic and structural numerical calculation and examples deriving from this new approach will be presented.
Design of a Low-Cost Easy-to-Fly STOL Ultralight Aircraft in Composite Material / Coiro, Domenico; Nicolosi, Fabrizio; DE MARCO, Agostino; N., Genito; S., Figliolia. - In: ACTA POLYTECHNICA. - ISSN 1210-2709. - STAMPA. - 45:N. 4 /2005(2005), pp. 73-80.
Design of a Low-Cost Easy-to-Fly STOL Ultralight Aircraft in Composite Material
COIRO, DOMENICO;NICOLOSI, FABRIZIO;DE MARCO, AGOSTINO;
2005
Abstract
The paper will deal with the design of the aircraft, starting from a market survey, conceptual design loop and preliminary choice of dimensions up to detailed design of an efficient high-lift systems and low-drag fuselage shape. Technological challenges regarding the design of low-cost systems for the flap/slat retraction and simple wing folding system will be highlighted. Aiming to an efficient optimization algorithm, it has been developed a new integration technique between CAD, aerodynamic and structural numerical calculation and examples deriving from this new approach will be presented.| File | Dimensione | Formato | |
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