Introduction to Optimization Methods and Tools for Multidisciplinary Design in Aeronautics and Turbomachinery PDF Download
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Author: Jacques Periaux
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 624
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Book Description
Author: Jacques Periaux
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 624
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Book Description
Author: H. Deconinck
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: H. Deconinck
Publisher:
ISBN: 9782930389561
Category : Aeronautics
Languages : en
Pages : 555
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Book Description
Author: Jacques Periaux
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590
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Book Description
Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN: 9782875160737
Category : Aerodynamics
Languages : en
Pages :
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Book Description
Author: Jacques Periaux
Publisher:
ISBN: 9782875160324
Category : Aerodynamics
Languages : en
Pages : 600
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Book Description
Author: Jacques Periaux
Publisher:
ISBN: 9782875160096
Category : Aerodynamics
Languages : en
Pages :
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Book Description
Author: Jacques Periaux
Publisher: Springer
ISBN: 9789401795197
Category : Technology & Engineering
Languages : en
Pages : 305
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Book Description
Many complex aeronautical design problems can be formulated with efficient multi-objective evolutionary optimization methods and game strategies. This book describes the role of advanced innovative evolution tools in the solution, or the set of solutions of single or multi disciplinary optimization. These tools use the concept of multi-population, asynchronous parallelization and hierarchical topology which allows different models including precise, intermediate and approximate models with each node belonging to the different hierarchical layer handled by a different Evolutionary Algorithm. The efficiency of evolutionary algorithms for both single and multi-objective optimization problems are significantly improved by the coupling of EAs with games and in particular by a new dynamic methodology named “Hybridized Nash-Pareto games”. Multi objective Optimization techniques and robust design problems taking into account uncertainties are introduced and explained in detail. Several applications dealing with civil aircraft and UAV, UCAV systems are implemented numerically and discussed. Applications of increasing optimization complexity are presented as well as two hands-on test cases problems. These examples focus on aeronautical applications and will be useful to the practitioner in the laboratory or in industrial design environments. The evolutionary methods coupled with games presented in this volume can be applied to other areas including surface and marine transport, structures, biomedical engineering, renewable energy and environmental problems. This book will be of interest to students, young scientists and engineers involved in the field of multi physics optimization.
Author: Marco Cavazzuti
Publisher: Springer Science & Business Media
ISBN: 3642311865
Category : Technology & Engineering
Languages : en
Pages : 272
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Book Description
This book is about optimization techniques and is subdivided into two parts. In the first part a wide overview on optimization theory is presented. Optimization is presented as being composed of five topics, namely: design of experiment, response surface modeling, deterministic optimization, stochastic optimization, and robust engineering design. Each chapter, after presenting the main techniques for each part, draws application oriented conclusions including didactic examples. In the second part some applications are presented to guide the reader through the process of setting up a few optimization exercises, analyzing critically the choices which are made step by step, and showing how the different topics that constitute the optimization theory can be used jointly in an optimization process. The applications which are presented are mainly in the field of thermodynamics and fluid dynamics due to the author's background.
Author: V. Panchenko
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
The gas turbine engine is a complex aerodynamic machine with performance, structural and manufacturability challenges. This paper gives an overview of a multidisciplinary optimization approach applied to the conceptual design of small aircraft engines. A description of major turbomachinery disciplines and the numerous interactions between disciplines is given followed by a discussion of the need for preliminary design optimization. The approach to development of such a system undertaken at Pratt & Whitney Canada is described including identification of appropriate design tools and their influence on the geometrical definition of an engine cross-section. Finally, preliminary optimization results are presented.
