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OverviewFull Product DetailsAuthor: Lorrie MolentPublisher: Springer Verlag, Singapore Imprint: Springer Verlag, Singapore Edition: 1st ed. 2024 Weight: 0.136kg ISBN: 9789819974672ISBN 10: 9819974674 Pages: 64 Publication Date: 19 December 2023 Audience: Professional and scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Manufactured on demand  We will order this item for you from a manufactured on demand supplier. Table of ContentsIntroduction.- Fatigue Demystified.- Some Design Considerations.- Lead Cracks and Simplified Lifing Methods.- Derivative Fatigue Crack Growth Models.- Fatigue Nucleating Discontinuities.- Lead Crack Lifing Methodology.- Fleet Management, Repair and Life Enhancement Considerations.- Concluding Remarks.- AcknowledgementsReviewsAuthor InformationMr. Lorrie Molent is an acknowledged authority in the fields of aircraft structural integrity, structural mechanics, structural and fatigue testing, advanced composite bonded repair, aircraft vulnerability, and aircraft accident investigation. He has more than 280 publications in these technical areas. Mr. Molent is a qualified aircraft accident investigator. He has been attached to both the then Australian Civil Aviation Department and the US Navy NAVAIR Structures in Washington D.C. as an airworthiness engineer and has a broad network of collaborators nationally and internationally. Until October 2020, Mr. Molent was the Australia’s Defence Science and Technology Group’s Head of Emerging Aircraft Structural Integrity. In 2010, he was presented with the Minister’s Award for Achievements in Defence Science, and he was awarded with a member of the Order of Australia (AM) in 2016. He also has numerous other team achievement awards. Currently, he works as a consultant and trainer in aircraft structural integrity, air accident investigation, and novel fatigue analyses methods. Tab Content 6Author Website:Countries AvailableAll regions |
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