Accurate characterisation of the fracture toughness of thin-sheet aluminum alloys is important to flaw-damage tolerant design of aerospace components such as airframes. For the next generation High Speed Civil Transport, the toughness of candidate aluminum alloy sheet is being evaluated by linear elastic resistance curves determined from wide-panel, middle-cracked tension (M(T)) specimens, often according to the ASTM Standard Practice of R-curve Determination (Designation E 56192a). Use of the wide-panel M(T) specimen in alloy development is limited by the requirement for a large quantity of material and a high capacity load-frame. The plane-strain initiation fracture toughness and plane-stress stable crack growth resistance were determined with a single small compact tension (C(T)) specimen for each of three precipitation hardened aluminum alloy sheets (AA2024-T3, AA2519-T87 (+Mg+Ag), and AA2650-T6). Crack length was monitored precisely with direct current potential difference (DCPD) measurements, and specimen plasticity was accounted for with the J-integral. The DCPD technique resolves a small amount of crack-tip process-zone damage (equal 20 micron) that constitutes crack initiation under plane-strain constraint. Two measures of initiation toughness are calculated: the elastic-plastic fracture toughness detected by DCPD (JICi, KJICi) and the toughness based on ASTM Standard E 813 (JlCi, KJIC) High resolution of fracture initiation is necessary to obtain a lower bound initiation toughness, KJICi, because plane-strain constraint is present ahead of the fatigue pre-crack but is rapidly lost with crack extension in thin sheet. KJIC overestimates toughness due to constraint loss coupled with the offset blunting line definition of fracture initiation. The J-integral/DCPD method provides a reproducible measure of the plane-stress linear elastic resistance curve (KJ - delta a) that compares reasonably to R-curves determined for large middle-cracked tension specimens. The small specimen method is effective for studies pertaining to alloy development, environmental effects, and fracture mechanisms.


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    Titel :

    High resolution R-curve characterization of the fracture toughness of thin sheet aluminum alloys


    Weitere Titelangaben:

    Charakterisierung der R-Kurve der Bruchzähigkeit von Blechen oder Grobblechen der Aluminiumlegierungen AA2024-T3, AA2519-T87 und AA2650


    Beteiligte:
    Haynes, M.J. (Autor:in) / Gangloff, R.P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1997


    Format / Umfang :

    17 Seiten, 13 Bilder, 3 Tabellen, 33 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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    Fracture toughness in titanium alloys

    Keller, R. / Chesnutt, J.C. / Froes, F.H. et al. | Tema Archiv | 1978


    Evolution of Microstructures, Fracture Toughness, and Fatigue Resistance During Processing of 7X50 Aluminum Alloys

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