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    Design and modeling of selective reinforcements for integral aircraft structures

    Boscolo, Marco / Allegri, Giuliano / Zhang, Xiang | Tema Archiv | 2008
    A numerical simulation is presented in this paper on the performance of crack retarders bonded to integral metallic structures. The work is ...

    Comparative study of corrosion-fatigue in aircraft materials

    Wang, Q.Y. / Pidaparti, R.M. / Palakal, M.J. | Tema Archiv | 2001
    Corrosion-fatigue is one of the damage mechanisms affecting the structural integrity of the aging aircraft. Simple analytical and ...

    Computational fluid dynamics driven optimization of blended wing body aircraft

    Peigin, Sergey / Epstein, Boris | Tema Archiv | 2006
    Aircraft', Journal of the Royal Aeronautical Society, Vol. 51, 1947, pp. 481-510). The BWB configuration concept is a radical change from the ...

    Optimization of aircraft wings for gust loads: interval analysis-based approach

    Rao, S.S. / Majumder, Luna | Tema Archiv | 2008
    An interval-based approach is presented for the optimization of aircraft structures under dynamic loads. As a specific application, the ...

    Correction to: Aircraft noise generation and assessment

    Bertsch, L. / Snellen, M. / Enghardt, L. et al. | Online Contents | 2019
    The original version of below mentioned articles was unfortunately published with the special issue titleAircraft noise generation and ...

    Framework for aircraft conceptual design and environmental performance studies

    Antoine, Nicolas E. / Kroo, Ilan M. | Tema Archiv | 2005
    Although civil aircraft environmental performance has been important since the beginnings of commercial aviation, continuously increasing ...

    Efficient approach for multipoint aerodynamic wing design of business jet aircraft

    Epstein, Boris / Peigin, Sergey | Tema Archiv | 2007
    design of three-dimensional isolated wings. In the framework of the method, the total drag of an optimized aircraft configuration is minimized at ...

    Extension to the Messinger model for aircraft icing

    Myers, T.G. | Tema Archiv | 2001
    a function of time, the ambient conditions, and the ice thickness. When glaze ice forms, the energy equation and mass balance are combined ...

    Low-frequency acoustic shielding by the silent aircraft airframe

    Agarwal, Anurag / Dowling, Ann P. | Tema Archiv | 2007
    The 'Silent Aircraft Initiative' is a project funded by the Cambridge-MIT Institute (CMI). Its aim is to discover ways of reducing aircraft ...

    Intergrid transformation for aircraft aerolastic simulations

    Badcock, K.J. / Rampurawala, A.M. / Richards, B.E. | Tema Archiv | 2004
    This Note considers the generalization of a transformation method for passing information between structural and aerodynamic surface grids ...