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Volumn 26, Issue 1, 2004, Pages 1-15

Fatigue crack growth in the aluminium alloy D16 under constant and variable amplitude loading

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; COMPUTER SIMULATION; CRACK PROPAGATION; STRESS ANALYSIS;

EID: 0242658552     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(03)00067-7     Document Type: Article
Times cited : (109)

References (32)
  • 1
    • 0242556017 scopus 로고
    • Full-scale fatigue testing of aircraft structures
    • Oxford: Pergamon Press
    • Plantema FJ, Schijve J, editor. Full-scale fatigue testing of aircraft structures. Proc Symp Amsterdam 1959. Oxford: Pergamon Press; 1961.
    • (1961) Proc Symp Amsterdam , vol.1959
    • Plantema, F.J.1    Schijve, J.2
  • 2
    • 85169428584 scopus 로고
    • Estimation of fatigue performance of aircraft structures
    • Fatigue of aircraft structures. Philadelphia, PA: ASTM
    • Schijve J. Estimation of fatigue performance of aircraft structures. Fatigue of aircraft structures, ASTM-STP 338. 1963;193-215 ASTM, Philadelphia, PA.
    • (1963) ASTM-STP , vol.338 , pp. 193-215
    • Schijve, J.1
  • 5
    • 0019655693 scopus 로고
    • Shear lips on fatigue fractures in aluminium sheet material
    • Schijve J. Shear lips on fatigue fractures in aluminium sheet material. Eng Fract Mech. 14:1981;789-800.
    • (1981) Eng Fract Mech , vol.14 , pp. 789-800
    • Schijve, J.1
  • 7
    • 0242556012 scopus 로고
    • The effect of sheet thickness on the fatigue crack propagation in 2024-T3 Alclad sheet material
    • Nat. Aerospace Lab. NLR, Amsterdam
    • Broek D, Schijve J. The effect of sheet thickness on the fatigue crack propagation in 2024-T3 Alclad sheet material. Nat. Aerospace Lab. NLR, Amsterdam, Tech. Report M.2129, 1963.
    • (1963) Tech. Report , vol.M.2129
    • Broek, D.1    Schijve, J.2
  • 8
    • 0019398428 scopus 로고
    • Some formulas for the crack opening stress level
    • Schijve J. Some formulas for the crack opening stress level. Eng Fract Mech. 14:1981;461-465.
    • (1981) Eng Fract Mech , vol.14 , pp. 461-465
    • Schijve, J.1
  • 9
    • 0001673801 scopus 로고
    • Fatigue crack propagation in light alloy sheet material and structures
    • Pergamon Press
    • Schijve J. Fatigue crack propagation in light alloy sheet material and structures. Advances in aeronautical sciences, vol. 3. 1961;387-408 Pergamon Press.
    • (1961) Advances in Aeronautical Sciences , vol.3 , pp. 387-408
    • Schijve, J.1
  • 10
    • 0008702822 scopus 로고    scopus 로고
    • Fatigue crack growth behaviour of 18G2A steel under constant amplitude loading and following a single overload
    • Skorupa M., Skorupa A., Schijve J., Machniewicz T., Korbut P. Fatigue crack growth behaviour of 18G2A steel under constant amplitude loading and following a single overload. The Archive of Mech Eng. 47:(1):2000;139-163.
    • (2000) The Archive of Mech Eng , vol.47 , Issue.1 , pp. 139-163
    • Skorupa, M.1    Skorupa, A.2    Schijve, J.3    Machniewicz, T.4    Korbut, P.5
  • 11
    • 0015462394 scopus 로고
    • Effect of multiple overloads on fatigue crack propagation in 2024-T3 aluminum alloy
    • Progress in flaw growth and fracture toughness testing, Philadelphia, PA: ASTM
    • Trebules V.W., Roberts R., Hertzberg R.W. Effect of multiple overloads on fatigue crack propagation in 2024-T3 aluminum alloy. Progress in flaw growth and fracture toughness testing, ASTM STP 536. 1973;115-146 ASTM, Philadelphia, PA.
    • (1973) ASTM STP , vol.536 , pp. 115-146
    • Trebules, V.W.1    Roberts, R.2    Hertzberg, R.W.3
  • 12
    • 0015055746 scopus 로고
    • The significance of fatigue crack closure
    • Damage tolerance in aircraft structures, Philadelphia, PA: ASTM
    • Elber W. The significance of fatigue crack closure. Damage tolerance in aircraft structures, ASTM STP 486. 1971;230-242 ASTM, Philadelphia, PA.
    • (1971) ASTM STP , vol.486 , pp. 230-242
    • Elber, W.1
  • 13
    • 0242640748 scopus 로고
    • The effect of 'ground-to-air' cycles on the fatigue crack propagation in 2024-T3 Alclad sheet material
    • Nat. Aerospace Lab. NLR, Amsterdam
    • Schijve J, De Rijk P. The effect of 'ground-to-air' cycles on the fatigue crack propagation in 2024-T3 Alclad sheet material. Nat. Aerospace Lab. NLR, Amsterdam, Tech. Report M.2148, 1965.
    • (1965) Tech. Report , vol.M.2148
    • Schijve, J.1    De Rijk, P.2
  • 15
    • 0023531710 scopus 로고
    • Crack propagation studies on Al 7475 on the basis of constant amplitude and selective variable amplitude loading histories
    • Zhang S., Marissen R., Schulte K., Trautmann K.K., Nowack H., Schijve J. Crack propagation studies on Al 7475 on the basis of constant amplitude and selective variable amplitude loading histories. Fatigue Fract Eng Mater Struct. 10:1987;315-332.
    • (1987) Fatigue Fract Eng Mater Struct , vol.10 , pp. 315-332
    • Zhang, S.1    Marissen, R.2    Schulte, K.3    Trautmann, K.K.4    Nowack, H.5    Schijve, J.6
  • 16
    • 0041749357 scopus 로고
    • Crack growth retardation due to intermittent overloads
    • Vardar Ö., Jildirim N. Crack growth retardation due to intermittent overloads. Int J Fatigue. 12:1990;283-287.
    • (1990) Int J Fatigue , vol.12 , pp. 283-287
    • Vardar, Ö.1    Jildirim, N.2
  • 17
    • 0032629834 scopus 로고    scopus 로고
    • The significance of fractography for investigations of fatigue crack growth under variable-amplitude loading
    • Schijve J. The significance of fractography for investigations of fatigue crack growth under variable-amplitude loading. Fatigue Fract Eng Mater Struct. 22:1999;87-99.
    • (1999) Fatigue Fract Eng Mater Struct , vol.22 , pp. 87-99
    • Schijve, J.1
  • 18
    • 85167410670 scopus 로고
    • Analysis of crack opening behavior by application of a discretized strip yield model
    • Mechanics of fatigue crack closure, Philadelphia, PA: ASTM
    • De Koning A.U., Liefting G. Analysis of crack opening behavior by application of a discretized strip yield model. Mechanics of fatigue crack closure, ASTM STP 982. 1988;437-458 ASTM, Philadelphia, PA.
    • (1988) ASTM STP , vol.982 , pp. 437-458
    • De Koning, A.U.1    Liefting, G.2
  • 19
    • 0242725130 scopus 로고    scopus 로고
    • Computer simulation of crack growth in steels under variable amplitude loading using a strip yield model
    • Quarterly of University of Mining & Metallurgy in Cracow
    • Skorupa M., Skorupa A., Zachwieja A. Computer simulation of crack growth in steels under variable amplitude loading using a strip yield model. Mechanika. Quarterly of University of Mining & Metallurgy in Cracow. 15:1996;443-456.
    • (1996) Mechanika , vol.15 , pp. 443-456
    • Skorupa, M.1    Skorupa, A.2    Zachwieja, A.3
  • 21
    • 0006892165 scopus 로고
    • The significance of cladding for fatigue of aluminium alloys in aircraft structures
    • National Aerospace Laboratory NLR, Amsterdam
    • Schijve J, Jacobs FA, Tromp J. The significance of cladding for fatigue of aluminium alloys in aircraft structures. National Aerospace Laboratory NLR, Amsterdam, Tech. Report 76065, 1976.
    • (1976) Tech. Report 76065
    • Schijve, J.1    Jacobs, F.A.2    Tromp, J.3
  • 22
    • 0019687589 scopus 로고
    • Evaluation of crack growth gages for service life tracking
    • Fracture mechanics, 13th Conference, Philadelphia, PA: ASTM
    • Saff C.R., Holloway D.R. Evaluation of crack growth gages for service life tracking. Fracture mechanics, 13th Conference, ASTM STP 743. 1981;623-640 ASTM, Philadelphia, PA.
    • (1981) ASTM STP , vol.743 , pp. 623-640
    • Saff, C.R.1    Holloway, D.R.2
  • 23
    • 0038046011 scopus 로고
    • The transition of fatigue cracks in Alclad sheet
    • National Aerospace Laboratory, NLR, Amsterdam
    • Broek D, De Rijk P, Sevenhuysen PJ. The transition of fatigue cracks in Alclad sheet. National Aerospace Laboratory, NLR, Amsterdam, Tech. Report M.2100, 1962.
    • (1962) Tech. Report , vol.M.2100
    • Broek, D.1    De Rijk, P.2    Sevenhuysen, P.J.3
  • 24
    • 0242725134 scopus 로고
    • The effect of the sheet width on the fatigue crack propagation in 2024-T3 Alclad material
    • National Aerospace Laboratory, NLR, Amsterdam
    • Schijve J, Nederveen A, Jacobs FA. The effect of the sheet width on the fatigue crack propagation in 2024-T3 Alclad material. National Aerospace Laboratory, NLR, Amsterdam, Tech. Report M.2142, 1965.
    • (1965) Tech. Report , vol.M.2142
    • Schijve, J.1    Nederveen, A.2    Jacobs, F.A.3
  • 25
    • 85003353720 scopus 로고
    • Crack propagation in clad 7079-T6 aluminum alloy sheet under constant and random amplitude fatigue loading
    • Fatigue crack propagation, Philadelphia, PA: ASTM
    • Swanson S.R., Cicci F., Hoppe W. Crack propagation in clad 7079-T6 aluminum alloy sheet under constant and random amplitude fatigue loading. Fatigue crack propagation, ASTM STP 415. 1967;312-362 ASTM, Philadelphia, PA.
    • (1967) ASTM STP , vol.415 , pp. 312-362
    • Swanson, S.R.1    Cicci, F.2    Hoppe, W.3
  • 26
    • 0019655693 scopus 로고
    • Shear lips on fatigue fractures in aluminium sheet material
    • Schijve J. Shear lips on fatigue fractures in aluminium sheet material. Eng Fract Mech. 14:1981;789-800.
    • (1981) Eng Fract Mech , vol.14 , pp. 789-800
    • Schijve, J.1
  • 28
    • 0016102363 scopus 로고
    • Fatigue damage accumulation and incompatible crack front orientation
    • Schijve J. Fatigue damage accumulation and incompatible crack front orientation. Eng Fract Mech. 6:1974;245-252.
    • (1974) Eng Fract Mech , vol.6 , pp. 245-252
    • Schijve, J.1
  • 31
    • 0032140477 scopus 로고    scopus 로고
    • Load interaction effects during fatigue crack growth under variable-amplitude loading. A literature review. Part I: Empirical trends
    • Skorupa M. Load interaction effects during fatigue crack growth under variable-amplitude loading. A literature review. Part I: Empirical trends. Fatigue Fract Eng Mater Struct. 21:1998;987-1006.
    • (1998) Fatigue Fract Eng Mater Struct , vol.21 , pp. 987-1006
    • Skorupa, M.1
  • 32
    • 0033209934 scopus 로고    scopus 로고
    • Load interaction effects during fatigue crack growth under variable-amplitude loading. A literature review. Part II: Qualitative interpretation
    • Skorupa M. Load interaction effects during fatigue crack growth under variable-amplitude loading. A literature review. Part II: Qualitative interpretation. Fatigue Fract Eng Mater Struct. 22:1999;905-926.
    • (1999) Fatigue Fract Eng Mater Struct , vol.22 , pp. 905-926
    • Skorupa, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.