Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties Tapa dura - 2012 - 2012th Edición
de Andrzej Skorupa; Malgorzata Skorupa
Descripción de contraportada
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.
Detalles
- Título Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties
- Autor Andrzej Skorupa; Malgorzata Skorupa
- Encuadernación Tapa dura
- Número de edición 2012th
- Edición 2012
- Páginas 332
- Volúmenes 1
- Idioma ENG
- Editorial Springer
- Fecha de publicación 2012-06-24
- ISBN 9789400742819 / 9400742819
- Peso 1.47 libras (0.67 kg)
- Dimensiones 9.21 x 6.14 x 0.81 pulgadas (23.39 x 15.60 x 2.06 cm)
-
Temas
- Aspects (Academic): Science/Technology Aspects
- Dewey Decimal Code 629.134
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Riveted Lap Joints in Aircraft Fuselage : Design, Analysis and Properties
de Andrzej Skorupa
- Nuevo
- Tapa dura
- Estado
- Nuevo
- Encuadernación
- Hardcover
- ISBN 10 / ISBN 13
- 9789400742819 / 9400742819
- Cantidad disponible
- 872
- Librería
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Uxbridge, Greater London, United Kingdom
- Precio
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EUR 160.60EUR 9.58 enviando a USA
Mostrar detalles
Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties
de Skorupa, Andrzej/ Skorupa, Malgorzata
- Nuevo
- Tapa dura
- Estado
- Nuevo
- Encuadernación
- Hardcover
- ISBN 10 / ISBN 13
- 9789400742819 / 9400742819
- Cantidad disponible
- 2
- Librería
-
Exeter, Devon, United Kingdom
- Precio
-
EUR 205.56EUR 11.99 enviando a USA