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Titlebook: Variational Analysis and Aerospace Engineering: Mathematical Challenges for Aerospace Design; Contributions from a Giuseppe Buttazzo,Aldo F

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书目名称Variational Analysis and Aerospace Engineering: Mathematical Challenges for Aerospace Design
副标题Contributions from a
编辑Giuseppe Buttazzo,Aldo Frediani
视频video
概述Discusses the most advanced problems in engineering which require an extensive application of mathematics.Presents important mathematical methods applied in aerospace engineering.Addresses researchers
丛书名称Springer Optimization and Its Applications
图书封面Titlebook: Variational Analysis and Aerospace Engineering: Mathematical Challenges for Aerospace Design; Contributions from a Giuseppe Buttazzo,Aldo F
描述.This volume consists of papers presented at the Variational Analysis and Aerospace Engineering Workshop II held in Erice, Italy in September 2010 at the International School of Mathematics "Guido Stampacchia". The workshop provided a platform for aerospace engineers and mathematicians (from universities, research centers and industry) to discuss the advanced problems requiring an extensive application of mathematics. The presentations were dedicated to the most advanced subjects in engineering and, in particular to computational fluid dynamics methods, introduction of new materials, optimization in aerodynamics, structural optimization, space missions, flight mechanics, control theory and optimization, variational methods and applications, etc.. .This book will capture the interest of researchers from both academia and industry..
出版日期Conference proceedings 2012
关键词Aerodynamics; Computational Fluidodynamics; Flight Mechanics; Fracture Mechanics; Optimal Control Proble
版次1
doihttps://doi.org/10.1007/978-1-4614-2435-2
isbn_softcover978-1-4939-5198-7
isbn_ebook978-1-4614-2435-2Series ISSN 1931-6828 Series E-ISSN 1931-6836
issn_series 1931-6828
copyrightSpringer Science+Business Media, LLC 2012
The information of publication is updating

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Optimal Location of Support Points in the Kirchhoff Plate,s supported at certain points ..,…,.., that is, the deflexion .(.) satisfies the Sobolev point conditions .(..)=⋯=.(..)=0. The optimal location of the support points is discussed such that either the compliance functional or the minimal deflexion functional attains its minimum.
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The PrandtlPlane Configuration: Overview on Possible Applications to Civil Aviation,one to conceive many different aircrafts for both passenger and freighter aviation, ranging from small Unmanned Aerial Vehicles (UAVs) to very large civil aircrafts, much larger than the present largest ones; different engine and propulsion systems became possible in view of the so-called “green aviation” of the future.
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Mesh Adaptivity and Optimal Shape Design for Aerospace,s combined with optimal shape design. The adaptivity uses an adjoint which we can calculate either by discretization of the analytical formulae or by automatic differentiation. We discuss the validity of both approaches and show some results.
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Giuseppe Buttazzo,Aldo FredianiDiscusses the most advanced problems in engineering which require an extensive application of mathematics.Presents important mathematical methods applied in aerospace engineering.Addresses researchers
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