2014, ISBN: 9789400792678
Design, Analysis and Properties Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associ… Mehr…
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ISBN: 9789400792678
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2014, ISBN: 9400792670
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2012, ISBN: 9789400792678
*Riveted Lap Joints in Aircraft Fuselage* - Design Analysis and Properties. Auflage 2012 / Taschenbuch für 160.49 € / Aus dem Bereich: Bücher, Wissenschaft, Technik Medien > Bücher nein B… Mehr…
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2014, ISBN: 9789400792678
Design, Analysis and Properties Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associ… Mehr…
ISBN: 9789400792678
Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient … Mehr…
ISBN: 9789400792678
Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient … Mehr…
2014, ISBN: 9400792670
2012 Kartoniert / Broschiert Klassische Mechanik, Fertigungstechnik und Ingenieurwesen, Luft- und Raumfahrttechnik, aircraftengineering; aluminiumalloys; Fatigue; fuselagesystems; rivet… Mehr…
2012, ISBN: 9789400792678
*Riveted Lap Joints in Aircraft Fuselage* - Design Analysis and Properties. Auflage 2012 / Taschenbuch für 160.49 € / Aus dem Bereich: Bücher, Wissenschaft, Technik Medien > Bücher nein B… Mehr…
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Detailangaben zum Buch - Riveted Lap Joints in Aircraft Fuselage
EAN (ISBN-13): 9789400792678
ISBN (ISBN-10): 9400792670
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2014
Herausgeber: Springer Netherlands
Buch in der Datenbank seit 2014-08-13T16:32:46+02:00 (Vienna)
Detailseite zuletzt geändert am 2023-12-22T19:18:42+01:00 (Vienna)
ISBN/EAN: 9400792670
ISBN - alternative Schreibweisen:
94-007-9267-0, 978-94-007-9267-8
Alternative Schreibweisen und verwandte Suchbegriffe:
Autor des Buches: skorupa, andrzej, malgorzata
Titel des Buches: aircraft, join, rive, riveted
Daten vom Verlag:
Autor/in: Andrzej Skorupa; Małgorzata Skorupa
Titel: Solid Mechanics and Its Applications; Riveted Lap Joints in Aircraft Fuselage - Design, Analysis and Properties
Verlag: Springer; Springer Netherland
332 Seiten
Erscheinungsjahr: 2014-07-18
Dordrecht; NL
Gedruckt / Hergestellt in Niederlande.
Sprache: Englisch
160,49 € (DE)
164,99 € (AT)
177,00 CHF (CH)
POD
XVI, 332 p.
BC; Hardcover, Softcover / Technik/Luftfahrttechnik, Raumfahrttechnik; Luft- und Raumfahrttechnik; Verstehen; aircraft engineering; aluminium alloys; fatigue; fuselage systems; riveted joints; riveting process; safety; Aerospace Technology and Astronautics; Industrial and Production Engineering; Classical Mechanics; Astronautik (Raumfahrttechnik); Fertigungstechnik und Ingenieurwesen; Klassische Mechanik; BB
Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient lifetime and safety, and formulating adequate inspection procedures. These aspects are all addressed in various formal protocols for creating and maintaining airworthiness, including damage tolerance considerations. In most transport aircraft, fatigue occurs in lap joints, sometimes leading to circumstances that threaten safety in critical ways. The problem of fatigue of lap joints has been considerably enlarged by the goal of extending aircraft lifetimes. Fatigue of riveted lap joints between aluminium alloy sheets, typical of the pressurized aircraft fuselage, is the major topic of the present book. The richly illustrated and well-structured chapters treat subjects such as: structural design solutions and loading conditions for fuselage skin joints; relevance of laboratory test results for simple lap joint specimens to riveted joints in a real structure; effect of various production and design related variables on the riveted joint fatigue behaviour; analytical and experimental results on load transmission in mechanically fastened lap joints; theoretical and experimental analysis of secondary bending and its implications for riveted joint fatigue performance; nucleation and shape development of fatigue cracks in riveted longitudinal lap joints; overview of experimental investigations into the multi-site damage for full scale fuselage panels and riveted lap joint specimens; fatigue crack growth and fatigue life prediction methodology for riveted lap joints; residual strength predictions for riveted lap joints in a fuselage structure. The major issues of each chapter are recapitulated in the last section.Provides help in rational planning of experiments on riveted lap joints in aircraft fuselage Provides essential information for safe in-service operation of aircrafts Includes 200 figures
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