Computerized Buckling Analysis of Shells

Bushnell, D.

ISBN 10: 9401087415 ISBN 13: 9789401087414
Verlag: Springer, 2014
Gebraucht Paperback

Verkäufer ThriftBooks-Dallas, Dallas, TX, USA Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

AbeBooks-Verkäufer seit 2. Juli 2009


Beschreibung

Beschreibung:

Pages can have notes/highlighting. Spine may show signs of wear. ~ ThriftBooks: Read More, Spend Less. Bestandsnummer des Verkäufers G9401087415I3N00

Diesen Artikel melden

Inhaltsangabe:

This report describes the work performed by Lockheed Palo Alto Research Labora­ tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini­ stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com­ pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways.

Críticas: `The book is a valuable contribution for engineers in government, industry, and universities who have complex shell buckling problems to solve and who have available to them computer programs for the buckling analysis of shells.'
Applied Mechanics Review, 38:8 (1986)
`What makes this book unique is that the author has succeeded in providing a `feel' for shell buckling based on careful mixture of theoretical, analytical, and numerical procedures. Many of the richly illustrated examples are written in a tutorial form, a guide-by-example for the modeling and solving of complex of nonlinear problems. It shows convincingly that the modern structural engineer must have a very thorough understanding of how structures behave if he is to use the advanced computational tools successfully. This book is a must for all those who work in the field of shell stability.'
Journal of Applied Mechanics, 53 (1986)

„Über diesen Titel“ kann sich auf eine andere Ausgabe dieses Titels beziehen.

Bibliografische Details

Titel: Computerized Buckling Analysis of Shells
Verlag: Springer
Erscheinungsdatum: 2014
Einband: Paperback
Zustand: Good
Zustand des Schutzumschlags: No Jacket

Beste Suchergebnisse bei AbeBooks

Foto des Verkäufers

D. Bushnell
Verlag: Springer Netherlands, 2014
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Softcover

Anbieter: moluna, Greven, Deutschland

Verkäuferbewertung 4 von 5 Sternen 4 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Zustand: New. Bestandsnummer des Verkäufers 5835251

Verkäufer kontaktieren

Neu kaufen

EUR 267,86
EUR 48,99 shipping
Versand von Deutschland nach USA

Anzahl: Mehr als 20 verfügbar

In den Warenkorb

Foto des Verkäufers

D. Bushnell
Verlag: Springer Netherland, 2014
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Taschenbuch

Anbieter: preigu, Osnabrück, Deutschland

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Taschenbuch. Zustand: Neu. Computerized buckling analysis of shells | D. Bushnell | Taschenbuch | xvii | Englisch | 2014 | Springer Netherland | EAN 9789401087414 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu. Bestandsnummer des Verkäufers 105330070

Verkäufer kontaktieren

Neu kaufen

EUR 277,75
EUR 70,00 shipping
Versand von Deutschland nach USA

Anzahl: 5 verfügbar

In den Warenkorb

Foto des Verkäufers

D. Bushnell
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Taschenbuch
Print-on-Demand

Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Taschenbuch. Zustand: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, 'Basic Research in Behavior of Metallic and Composite Components of Airframe Structures'. The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 448 pp. Englisch. Bestandsnummer des Verkäufers 9789401087414

Verkäufer kontaktieren

Neu kaufen

EUR 320,99
EUR 60,00 shipping
Versand von Deutschland nach USA

Anzahl: 1 verfügbar

In den Warenkorb

Foto des Verkäufers

D. Bushnell
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Taschenbuch

Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Taschenbuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, 'Basic Research in Behavior of Metallic and Composite Components of Airframe Structures'. The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways. Bestandsnummer des Verkäufers 9789401087414

Verkäufer kontaktieren

Neu kaufen

EUR 331,86
EUR 63,37 shipping
Versand von Deutschland nach USA

Anzahl: 1 verfügbar

In den Warenkorb

Beispielbild für diese ISBN

Bushnell, D.
Verlag: Springer, 2014
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Softcover

Anbieter: California Books, Miami, FL, USA

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Zustand: New. Bestandsnummer des Verkäufers I-9789401087414

Verkäufer kontaktieren

Neu kaufen

EUR 370,92
Versand gratis
Versand innerhalb von USA

Anzahl: Mehr als 20 verfügbar

In den Warenkorb

Foto des Verkäufers

D. Bushnell
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Taschenbuch
Print-on-Demand

Anbieter: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Deutschland

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, 'Basic Research in Behavior of Metallic and Composite Components of Airframe Structures'. The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways. 448 pp. Englisch. Bestandsnummer des Verkäufers 9789401087414

Verkäufer kontaktieren

Neu kaufen

EUR 392,69
EUR 23,00 shipping
Versand von Deutschland nach USA

Anzahl: 2 verfügbar

In den Warenkorb

Beispielbild für diese ISBN

Bushnell, D.
Verlag: Springer Verlag, 2014
ISBN 10: 9401087415 ISBN 13: 9789401087414
Neu Paperback

Anbieter: Revaluation Books, Exeter, Vereinigtes Königreich

Verkäuferbewertung 5 von 5 Sternen 5 Sterne, Erfahren Sie mehr über Verkäufer-Bewertungen

Paperback. Zustand: Brand New. 1989 edition. 450 pages. 9.25x6.10x0.73 inches. In Stock. Bestandsnummer des Verkäufers x-9401087415

Verkäufer kontaktieren

Neu kaufen

EUR 442,67
EUR 14,23 shipping
Versand von Vereinigtes Königreich nach USA

Anzahl: 2 verfügbar

In den Warenkorb