Automatic shape optimization using parametric CAD applied to sonic boom reduction-Reference-Cited by-同舟云学术

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Automatic shape optimization using parametric CAD applied to sonic boom reduction

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Daumas Laurent¹,Dinh Quang¹,Kleinveld Steven¹,Rogé Gilbert¹

Affiliation:

1. Dassault Aviation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1919

Reference5 articles.

1. 1J.L.Lions,Contrôleoptimaldessystèmesgouvernéspardeséquationsauxdérivéespartielles,Dunod,Paris,1968.

2. L.Daumas, Q.V.Dinh, S.Kleinveld and G.Rogé. Impact of automatic optimization in the design process of supersonic businessjet,Design Optimization International Conference, March31 -April 22004,Athens,Greece

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Discrete Adjoint Optimization Method for Low-Boom Aircraft Design Using Equivalent Area Distribution;Aerospace;2024-07-03

2. Inverse Design of Low-Boom Supersonic Concepts Using Reversed Equivalent-Area Targets;Journal of Aircraft;2014-01

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