2010, ISBN: 3838332512

[EAN: 9783838332512], Neubuch, [PU: LAP LAMBERT Academic Publishing], nach der Bestellung gedruckt Neuware - Printed after ordering - Aerospace structures are usually operated in extreme … Más…

[EAN: 9783838332512], Neubuch, [PU: LAP LAMBERT Academic Publishing], nach der Bestellung gedruckt Neuware - Printed after ordering - 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., Books<

2012, ISBN: 9783838332512

[ED: Taschenbuch], [PU: LAP LAMBERT Academic Publishing], Neuware - Aerospace structures are usually operated in extreme and uncertain environment, and subject to the requirements of mini… Más…

[ED: Taschenbuch], [PU: LAP LAMBERT Academic Publishing], 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., DE, [SC: 15.00], Neuware, gewerbliches Angebot, 220x150x20 mm, 324, [GW: 500g], Banküberweisung, PayPal, Internationaler Versand<

2009, ISBN: 3838332512

[EAN: 9783838332512], Neubuch, [PU: LAP LAMBERT Academic Publishing Dez 2009], This item is printed on demand - it takes 3-4 days longer - Neuware -Aerospace structures are usually operat… Más…

[EAN: 9783838332512], Neubuch, [PU: LAP LAMBERT Academic Publishing Dez 2009], This item is printed on demand - it takes 3-4 days longer - 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. 324 pp. Englisch, Books<

ISBN: 9783838332512

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… Más…

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. New Textbooks>Trade Paperback>Science>Engineering>Mech Engr, LAP Lambert Academic Publishing Core >1 >T<

2009, ISBN: 3838332512

[EAN: 9783838332512], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestell… Más…

[EAN: 9783838332512], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. 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 t., Books<