Department of Aircraft Design - ITA

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Aircraft Design Department Airplane design • MATLAB® framework Airplane Machine • Transport aircraft only • Performance calculation • Configuration parameters (seating abreast; wing location, engine location, number of aisles, etc…) • Engine and airplane can be designed simultaneously • Noise signature and emission profile • Wing airfoils design integration into current framework • Consideration of wingtip devices • Enable assessment of new technology • Tail surfaces designed by static and dynamic stability criteria (no tail volume coefficient employed) • Aeroelasticity of flexible wings (under development)
Aircraft Design Department Airplane design Airplane Modeler - Fuselage - Variety of cross section (double deck, cargo compartment able to accommodate any sort of containers) - Windshield with single or double curvature - Assement of outside view area for the pilot - Variety of tail cone shapes
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Aircraft Design Department Comparat
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Aircraft Design Department ANN appl
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Framework for Conceptual Design of
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Department of Aircraft Design - ITA

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