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000839469 019__ $$a1038055198
000839469 020__ $$a9789811083990$$q(electronic book)
000839469 020__ $$a9811083991$$q(electronic book)
000839469 020__ $$z9789811083983
000839469 020__ $$z9811083983
000839469 035__ $$aSP(OCoLC)on1037946080
000839469 035__ $$aSP(OCoLC)1037946080$$z(OCoLC)1038055198
000839469 040__ $$aN$T$$beng$$erda$$epn$$cN$T$$dGW5XE$$dN$T$$dEBLCP$$dYDX$$dAZU$$dUAB$$dOCLCF$$dOCLCQ
000839469 049__ $$aISEA
000839469 050_4 $$aTL671.6
000839469 08204 $$a629.134/31$$223
000839469 1001_ $$aLiu, Jun,$$eauthor.
000839469 24510 $$aLong-life design and test technology of typical aircraft structures /$$cJun Liu, Zhufeng Yue, Xiaoliang Geng, Shifeng Wen, Wuzhu Yan.
000839469 264_1 $$aSingapore :$$bSpringer,$$c2018.
000839469 300__ $$a1 online resource
000839469 336__ $$atext$$btxt$$2rdacontent
000839469 337__ $$acomputer$$bc$$2rdamedia
000839469 338__ $$aonline resource$$bcr$$2rdacarrier
000839469 504__ $$aIncludes bibliographical references.
000839469 5050_ $$aIntro; Preface; Contents; Brief Introduction; 1 Introduction; References; 2 Outline of Fatigue and Fracture Mechanics; 2.1 Basic Conception of Fatigue; 2.1.1 Definition of Fatigue and Its Damage Property; 2.1.2 Alternating Stress; 2.1.3 Curve S-N; 2.1.4 Equal-Life Curve; 2.1.5 Stress Fatigue and Strain Fatigue; 2.1.6 Linear Cumulative Damage Theory; 2.2 The Main Factors that Affect the Structural Fatigue Performance; 2.2.1 Effects of Load Spectrum; 2.2.2 Effects of Stress Concentration; 2.2.3 Effects of Size; 2.2.4 Effects of Surface Roughness and Residual Stress
000839469 5058_ $$a2.3 Mechanism of Fatigue Failure, Crack Propagation, and Fracture Analysis of Metals2.3.1 Mechanism of Fatigue Failure; 2.3.2 Fatigue Crack Propagating Theory; 2.3.3 Fractographic Analysis; 2.4 Estimate Methods of Fatigue Life; 2.4.1 Nominal Stress Approach; 2.4.2 Local Stress-Strain Method; 2.4.3 Multiaxial Fatigue Theory; References; 3 Effect of Surface Quality of Open Holes on Fatigue Life; 3.1 Effect of the Surface Defects on Fatigue Life of Open Holes; 3.1.1 Scratch; 3.1.2 Cavity; 3.1.3 Inclusion; 3.2 Effect of Manufacturing Quality on Fatigue Performance of Open Holes
000839469 5058_ $$a3.2.1 Surface Roughness3.2.2 Verticality; 3.2.3 Cylindricity; 3.2.4 Roundness; 3.2.5 Manufacturing Quality of Fasten Holes and Empirical Equation; 3.3 Effect of Drilling on Fatigue Performance of Open Holes; 3.3.1 Specimen Size and Loading; 3.3.2 Fatigue Test Results; References; 4 Anti-fatigue Strengthening Technology of Holes; 4.1 Effect of Cold Expansion on Fatigue Performance of Open Holes; 4.1.1 Direct Mandrel Expansion Process and Its Parameters; 4.1.2 Residual Stress Measurements; 4.1.2.1 Tangential Residual Stress Distribution
000839469 5058_ $$a4.1.2.2 Tangential Residual Stress in Longitudinal and Transverse Distributions4.1.2.3 Layered Depth Distribution of Tangential Residual Stress; 4.1.3 Fatigue Test Results and Fracture Analysis; 4.1.4 FEM Analysis; 4.2 Effect of Impression on Fatigue Performance of Open Holes; 4.2.1 Impression Process; 4.2.2 Influence of Indenter Size on Residual Stress Distribution; 4.2.3 Influence of Different Factors on Residual Stress of Impression-Reinforced Holes; 4.2.3.1 Effect of Extrusion Amount on Residual Stress Distribution
000839469 5058_ $$a4.2.3.2 Effect of Friction Between Indenter and Specimen on Residual Stress Distribution4.2.3.3 Influence of Loading Sequence on Residual Stress Distribution; 4.2.4 Fatigue Test of Three-Hole Sample Impressed; 4.3 Effect of Hammering on Fatigue Performance of Open Hole; 4.3.1 Hammering and Fatigue Testing; 4.3.2 Finite Element Analysis of Hammering; 4.3.3 Fracture Analysis; References; 5 Shot Peening Strengthening Technology; 5.1 Mechanism of Shot Peening and Status of Art; 5.2 Effect of Shot Materials on Fatigue Performance; 5.2.1 Fatigue Test; 5.2.2 Comparative Analysis of Fatigue Test Data
000839469 506__ $$aAccess limited to authorized users.
000839469 520__ $$aThis 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 problems in aircraft engineering, it will benefit researchers and engineers in the fields of Aerospace Technology and Astronautics.
000839469 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed May 29, 2018).
000839469 650_0 $$aAirframes$$xFatigue.
000839469 650_0 $$aAirframes$$xDesign and construction.
000839469 7001_ $$aYue, Zhufeng,$$eauthor.
000839469 7001_ $$aGeng, Xiaoliang,$$eauthor.
000839469 7001_ $$aWen, Shifeng,$$eauthor.
000839469 7001_ $$aYan, Wuzhu,$$eauthor.
000839469 77608 $$iPrint version: $$z9811083983$$z9789811083983$$w(OCoLC)1020025392
000839469 852__ $$bebk
000839469 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-981-10-8399-0$$zOnline Access$$91397441.1
000839469 909CO $$ooai:library.usi.edu:839469$$pGLOBAL_SET
000839469 980__ $$aEBOOK
000839469 980__ $$aBIB
000839469 982__ $$aEbook
000839469 983__ $$aOnline
000839469 994__ $$a92$$bISE