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Multiobjective Optimization - LUNA MAJUMDER
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LUNA MAJUMDER:
Multiobjective Optimization - Taschenbuch

ISBN: 9783838332512

ID: 9783838332512

An interval analysis-based multiobjective optimization of supersonic wing structures Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure. Multiobjective Optimization: Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure., LAP Lambert Acad. Publ.

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Multiobjective Optimization - An interval analysis-based multiobjective optimization of supersonic wing structures
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Multiobjective Optimization - An interval analysis-based multiobjective optimization of supersonic wing structures - Taschenbuch

2010, ISBN: 9783838332512

[ED: Taschenbuch / Paperback], [PU: LAP Lambert Academic Publishing], Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure., [SC: 0.00], Neuware, gewerbliches Angebot

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Multiobjective Optimization - LUNA MAJUMDER
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LUNA MAJUMDER:
Multiobjective Optimization - Taschenbuch

ISBN: 9783838332512

[ED: Taschenbuch], [PU: LAP Lambert Acad. Publ.], Neuware - Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure. -, [SC: 0.00], Neuware, gewerbliches Angebot, 220x150x19 mm, [GW: 499g]

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Multiobjective Optimization - LUNA MAJUMDER
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LUNA MAJUMDER:
Multiobjective Optimization - Taschenbuch

ISBN: 9783838332512

[ED: Taschenbuch], [PU: LAP Lambert Acad. Publ.], Neuware - Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure., [SC: 0.00], Neuware, gewerbliches Angebot, 220x150x19 mm, [GW: 499g]

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ISBN: 9783838332512

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Multiobjective Optimization:An interval analysis-based multiobjective optimization of supersonic wing structures LUNA MAJUMDER Multiobjective Optimization:An interval analysis-based multiobjective optimization of supersonic wing structures LUNA MAJUMDER Bücher > Wissenschaft > Technik, LAP Lambert Acad. Publ.

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Details zum Buch
Multiobjective Optimization

Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of minimum weight, high performance and reliability. An interval-based game theory technique, coupled with interval-based nonlinear programming techniques is used for the optimum solution. The methodology is illustrated with two examples. The first one is a symmetric double wedge airfoil and the second one is a supersonic airplane wing. Three objectives, namely, the minimization of structural weight, minimization of energy and maximization of flutter Mach number for a specified flight condition are considered. The maximum stress, wing tip deflection, root angle of attack, natural frequencies and the stresses in the wing structure due to taxiing, gust and landing loads are suitably constrained. To deal with imprecision present in the system, probabilistic and interval approaches are used. Numerical examples are presented to illustrate the computational feasibility and effectiveness of the approaches. This work should be useful to students and researchers who are studying aerospace engineering during their preliminary design of an airplane structure.

Detailangaben zum Buch - Multiobjective Optimization


EAN (ISBN-13): 9783838332512
ISBN (ISBN-10): 3838332512
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2010
Herausgeber: LAP Lambert Academic Publishing

Buch in der Datenbank seit 02.12.2007 18:31:41
Buch zuletzt gefunden am 01.10.2017 08:28:17
ISBN/EAN: 9783838332512

ISBN - alternative Schreibweisen:
3-8383-3251-2, 978-3-8383-3251-2


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