000 03840nam a22005535i 4500
001 978-981-99-7468-9
003 DE-He213
005 20251030110856.0
007 cr nn 008mamaa
008 231218s2024 si | s |||| 0|eng d
020 _a9789819974689
_9978-981-99-7468-9
024 7 _a10.1007/978-981-99-7468-9
_2doi
050 4 _aTA401-492
072 7 _aTGM
_2bicssc
072 7 _aTEC021000
_2bisacsh
072 7 _aTGM
_2thema
100 1 _aMolent, Lorrie.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_968380
245 1 0 _aAircraft Fatigue Management
_h[electronic resource] /
_cby Lorrie Molent.
250 _a1st ed. 2024.
264 1 _aSingapore :
_bSpringer Nature Singapore :
_bImprint: Springer,
_c2024.
300 _aIX, 64 p. 20 illus., 17 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-5318
505 0 _aIntroduction -- 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 -- Acknowledgements.
520 _aFatigue occurs under cyclic loading and can significantly degrade the operational capability and safety of metallic aircraft components and structures. This book provides summaries of some metallic aircraft structural integrity issues, innovative but established examples of maintaining operational capability—airworthiness, and assessments of safe in-service fatigue lives. These topics are based on a through-life fatigue management philosophy that ensures safe and continued operation, including during life extensions that are almost inevitably required. This philosophy is underpinned by observations of the behaviour of fatigue cracks in actual structures subjected to realistic service loading conditions. The book includes topics like aircraft design requirements, individual aircraft fatigue loads monitoring, airframe fatigue testing, sources of fatigue-nucleating discontinuities, and prediction of fatigue crack growth from these discontinuities. All these aspects contribute to discussing methods of assuring the structural integrity and operational capability of realistically cracked structures. The book also discusses the exponential behaviour of lead or dominant cracks—those leading to first failure—and the practical significance of differences between fatigue fracture topographies produced under constant amplitude and variable amplitude loading. The book can be a valuable reference for researchers and professionals interested in aircraft fatigue management and allied fields.
650 0 _aBuilding materials.
650 0 _aAerospace engineering.
_966335
650 0 _aAstronautics.
_966336
650 0 _aMechanics, Applied.
650 0 _aSolids.
_965936
650 1 4 _aStructural Materials.
_965620
650 2 4 _aAerospace Technology and Astronautics.
_966339
650 2 4 _aSolid Mechanics.
_965938
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9789819974672
776 0 8 _iPrinted edition:
_z9789819974696
830 0 _aSpringerBriefs in Applied Sciences and Technology,
_x2191-5318
_965846
856 4 0 _uhttps://doi.org/10.1007/978-981-99-7468-9
912 _aZDB-2-CMS
912 _aZDB-2-SXC
999 _c56858
_d56858