Verwandte Artikel zu Automated Finite Element Modeling of Wing Structures...
Inhaltsangabe
The displacement formulation of the finite element method is the most general and most widely used technique for structural analysis of airplane configurations. Modem structural synthesis techniques based on the finite element method have reached a certain maturity in recent years, and large airplane structures can now be optimized with respect to sizing type design variables for many load cases subject to a rich variety of constraints including stress, buckling, frequency, stiffness and aeroelastic constraints (Refs. 1-3). These structural synthesis capabilities use gradient based nonlinear programming techniques to search for improved designs. For these techniques to be practical a major improvement was required in computational cost of finite element analyses (needed repeatedly in the optimization process). Thus, associated with the progress in structural optimization, a new perspective of structural analysis has emerged, namely, structural analysis specialized for design optimization application, or.what is known as "design oriented structural analysis" (Ref. 4). This discipline includes approximation concepts and methods for obtaining behavior sensitivity information (Ref. 1), all needed to make the optimization of large structural systems (modeled by thousands of degrees of freedom and thousands of design variables) practical and cost effective.
Die Inhaltsangabe kann sich auf eine andere Ausgabe dieses Titels beziehen.
Reseña del editor
The displacement formulation of the finite element method is the most general and most widely used technique for structural analysis of airplane configurations. Modem structural synthesis techniques based on the finite element method have reached a certain maturity in recent years, and large airplane structures can now be optimized with respect to sizing type design variables for many load cases subject to a rich variety of constraints including stress, buckling, frequency, stiffness and aeroelastic constraints (Refs. 1-3). These structural synthesis capabilities use gradient based nonlinear programming techniques to search for improved designs. For these techniques to be practical a major improvement was required in computational cost of finite element analyses (needed repeatedly in the optimization process). Thus, associated with the progress in structural optimization, a new perspective of structural analysis has emerged, namely, structural analysis specialized for design optimization application, or.what is known as "design oriented structural analysis" (Ref. 4). This discipline includes approximation concepts and methods for obtaining behavior sensitivity information (Ref. 1), all needed to make the optimization of large structural systems (modeled by thousands of degrees of freedom and thousands of design variables) practical and cost effective.
„Über diesen Titel“ kann sich auf eine andere Ausgabe dieses Titels beziehen.
- VerlagBiblioScholar
- Erscheinungsdatum2013
- ISBN 10 1288910045
- ISBN 13 9781288910045
- EinbandTapa blanda
- SpracheEnglisch
- Anzahl der Seiten186
- Kontakt zum HerstellerNicht verfügbar
EUR 103,96
EUR 29,69 für den Versand von Vereinigtes Königreich nach Deutschland
Versandziele, Kosten & DauerNeu kaufen
Diesen Artikel anzeigen
EUR 60,26
EUR 0,62 für den Versand von USA nach Deutschland
Versandziele, Kosten & DauerSuchergebnisse für Automated Finite Element Modeling of Wing Structures...
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Print-on-DemandAnbieter: PBShop.store US, Wood Dale, IL, USA
Verkäuferbewertung 5 von 5 Sternen
PAP. Zustand: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Bestandsnummer des Verkäufers L0-9781288910045
Anzahl: Mehr als 20 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Print-on-DemandAnbieter: PBShop.store UK, Fairford, GLOS, Vereinigtes Königreich
Verkäuferbewertung 4 von 5 Sternen
PAP. Zustand: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Bestandsnummer des Verkäufers L0-9781288910045
Anzahl: Mehr als 20 verfügbar
Foto des Verkäufers
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Anbieter: moluna, Greven, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Zustand: New. KlappentextrnrnThe displacement formulation of the finite element method is the most general and most widely used technique for structural analysis of airplane configurations. Modem structural synthesis techniques based on the finite element met. Bestandsnummer des Verkäufers 4085510
Anzahl: Mehr als 20 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Anbieter: Ria Christie Collections, Uxbridge, Vereinigtes Königreich
Verkäuferbewertung 5 von 5 Sternen
Zustand: New. In. Bestandsnummer des Verkäufers ria9781288910045_new
Anzahl: Mehr als 20 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Anbieter: Chiron Media, Wallingford, Vereinigtes Königreich
Verkäuferbewertung 5 von 5 Sternen
Paperback. Zustand: New. Bestandsnummer des Verkäufers 6666-IUK-9781288910045
Anzahl: 10 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Print-on-DemandAnbieter: THE SAINT BOOKSTORE, Southport, Vereinigtes Königreich
Verkäuferbewertung 5 von 5 Sternen
Paperback / softback. Zustand: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days 189. Bestandsnummer des Verkäufers C9781288910045
Anzahl: Mehr als 20 verfügbar
Foto des Verkäufers
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Verlag:
Creative Media Partners, LLC Mär 2013, 2013
ISBN 10: 1288910045
ISBN 13: 9781288910045
Neu
Taschenbuch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Verkäuferbewertung 5 von 5 Sternen
Taschenbuch. Zustand: Neu. Neuware - The displacement formulation of the finite element method is the most general and most widely used technique for structural analysis of airplane configurations. Modem structural synthesis techniques based on the finite element method have reached a certain maturity in recent years, and large airplane structures can now be optimized with respect to sizing type design variables for many load cases subject to a rich variety of constraints including stress, buckling, frequency, stiffness and aeroelastic constraints (Refs. 1-3). These structural synthesis capabilities use gradient based nonlinear programming techniques to search for improved designs. For these techniques to be practical a major improvement was required in computational cost of finite element analyses (needed repeatedly in the optimization process). Thus, associated with the progress in structural optimization, a new perspective of structural analysis has emerged, namely, structural analysis specialized for design optimization application, or.what is known as 'design oriented structural analysis' (Ref. 4). This discipline includes approximation concepts and methods for obtaining behavior sensitivity information (Ref. 1), all needed to make the optimization of large structural systems (modeled by thousands of degrees of freedom and thousands of design variables) practical and cost effective. Bestandsnummer des Verkäufers 9781288910045
Anzahl: 2 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Anbieter: Lucky's Textbooks, Dallas, TX, USA
Verkäuferbewertung 5 von 5 Sternen
Zustand: New. Bestandsnummer des Verkäufers ABLIING23Mar2411530033858
Anzahl: Mehr als 20 verfügbar
Beispielbild für diese ISBN
Automated Finite Element Modeling of Wing Structures for Shape Optimization
Anbieter: Mispah books, Redhill, SURRE, Vereinigtes Königreich
Verkäuferbewertung 4 von 5 Sternen
Paperback. Zustand: Like New. Like New. book. Bestandsnummer des Verkäufers ERICA79612889100456
Anzahl: 1 verfügbar