Automatic shape optimization using parametric CAD applied to sonic boom reduction

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2007, Pages 2671-2681

  Daumas, Laurent ^a   Dinh, Quang ^a   Kleinveld, Steven ^a   Rogé, Gilbert ^a  

^a Dassault Aviation   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTER AIDED DESIGN; CONSTRAINT THEORY; EULER EQUATIONS; INVERSE PROBLEMS;

CRUISE PERFORMANCE; MULTIDISCIPLINARY DESIGN; SONIC BOOM REDUCTION;

SHAPE OPTIMIZATION;

EID: 34547512635     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. J.-L. Lions, Contrôle optimal des systèmes gouvernés par des équations aux dérivées partielles, Dunod, Paris, 1968.
2. J. Herskovits, E. Lapporte, P. Le Tallec and . Santos, "A Quasi-Newton Interior Point Algorithm Applied for Constrained Optimum Design in Computational Fluid Dynamics", European Journal of Finite Elements, Vol.5, pp 595-617, Hermes, 1996.
3. Q.V. Dinh, G. Rogé, C. Sevin and B. Stoufflet, "Shape Optimisation in Computational Fluid Dynamics", European Journal of Finite Elements, Vol.5, pp 569-594, Hermes, 1996.
4. L.Daumas, Q.V.Dinh, S.Kleinveld and G.Rogé. Impact of automatic optimization in the design process of supersonic business jet, Design Optimization International Conference, March 31 - April 2 2004, Athens,Greece
5. L.Daumas, Q.V.Dinh, S.Kleinveld and G.Rogé. Winglet shape optimization with geometric constraints using a CAD modeler, 1rst International Conference on innovation and integration in aerospace sciences, 4-5 august 2005. Queen's university Belfast, Northern Ireland, UK, CEIAT 2005-0043