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L. Molent

The following bibliography contains all publications indexed in this database that are linked with this name as either author, editor or any other kind of contributor.

  1. Molent, L. / Callinan, R. J. / Jones, R. (1989): Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects. In: Composite Structures, v. 11, n. 1 ( 1989).

    https://doi.org/10.1016/0263-8223(89)90030-5

  2. Molent, L. / Bridgford, N. / Rees, D. / Jones, R. (1992): Environmental evaluation of repairs to fuselage lap joints. In: Composite Structures, v. 21, n. 2 ( 1992).

    https://doi.org/10.1016/0263-8223(92)90047-g

  3. Jones, R. / Molent, L. (2004): Application of constitutive modelling and advanced repair technology to F111C aircraft. In: Composite Structures, v. 66, n. 1-4 (October 2004).

    https://doi.org/10.1016/j.compstruct.2004.04.032

  4. Jones, R. / Barter, S. / Molent, L. / Pitt, S. (2005): Crack patching: an experimental evaluation of fatigue crack growth. In: Composite Structures, v. 67, n. 2 (February 2005).

    https://doi.org/10.1016/j.compstruct.2004.09.020

  5. Molent, L. / Haddad, A. (2020): A critical review of available composite damage growth test data under fatigue loading and implications for aircraft sustainment. In: Composite Structures, v. 232 (January 2020).

    https://doi.org/10.1016/j.compstruct.2019.111568

  6. Molent, L. / Forrester, C. (2017): The lead crack concept applied to defect growth in aircraft composite structures. In: Composite Structures, v. 166 (April 2017).

    https://doi.org/10.1016/j.compstruct.2016.12.076

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