Long-Life Design and Test Technology of Typical Aircraft Structures
This book addresses anti-fatigue manufacturing, analysis and test verification technologies for typical aircraft structures, including fastening holes, shot peening plates, different types of joints and wing boxes. Offering concrete solutions to practical
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ong-Life Design and Test Technology of Typical Aircraft Structures
Long-Life Design and Test Technology of Typical Aircraft Structures
Jun Liu Zhufeng Yue Xiaoliang Geng Shifeng Wen Wuzhu Yan •
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Long-Life Design and Test Technology of Typical Aircraft Structures
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Jun Liu School of Mechanics, Civil Engineering and Architecture Northwestern Polytechnical University Xi’an, Shaanxi China Zhufeng Yue Northwestern Polytechnical University Xi’an, Shaanxi China
Shifeng Wen Northwestern Polytechnical University Xi’an, Shaanxi China Wuzhu Yan Northwestern Polytechnical University Xi’an, Shaanxi China
Xiaoliang Geng Northwestern Polytechnical University Xi’an, Shaanxi China
ISBN 978-981-10-8398-3 ISBN 978-981-10-8399-0 https://doi.org/10.1007/978-981-10-8399-0
(eBook)
Jointly published with National Defense Industry Press, Beijing, China The print edition is not for sale in China Mainland. Customers from China Mainland please order the print book from: National Defense Industry Press. Library of Congress Control Number: 2018934954 © National Defense Industry Press and Springer Nature Singapore Pte Ltd. 2018 This work is subject to copyright. All rights are reserved by the Publishers, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. The publishers, the authors and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publishers nor the authors or the editors give a warranty, express or implied, with respect to the material contained herein or for any errors or omissions that may have been made. The publishers remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. Printed on acid-free paper This Springer imprint is published by the registered company Springer Nature Singapore Pte Ltd. part of Springer Nature The registered company address is: 152 Beach Road, #21-01/04 Gateway East, Singapore 189721, Singapore
Preface
Aviation technology is moving forward at an unprecedented speed. Aircraft structures tend to be large in scale, complex, lightweight, and sophisticated. However, the service environment of aircraft structures is getting worse. Its development increasingly focuses on improving reliability and reducing costs, that is, improving safety and extending material life under the premise of meeting structural strength requirements. Structural anti-fatigue
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