A parametric associative modelling of aeronautical structural concepts under C 0, C 1 or C 2 continuity constraints

Publisher: Cambridge University Press

E-ISSN: 2059-6464|116|1181|727-741

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.116, Iss.1181, 2012-07, pp. : 727-741

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Abstract