Search Results - Akbar, Mahesa

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  1. 1
    Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method

    Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method by Abdullah, Nur Azam, Curiel-Sosa, Jose Luis, Akbar, Mahesa

    Published 2018
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  2. 2
    Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method

    Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method by Abdullah, Nur Azam, Curiel-Sosa, Jose Luis, Akbar, Mahesa

    Published 2017
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  3. 3
    Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM

    Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM by Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L.

    Published 2018
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  4. 4
    Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM

    Structural integrity assessment on cracked composites interaction with aeroelastic constraint by means of XFEM by Abdullah, Nur Azam, Akbar, Mahesa, Wirawan, Nanda, Curiel-Sosa, Jose Luis

    Published 2019
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  5. 5
    Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM

    Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM by Abdullah, Nur Azam, Curiel-Sosa, J.L., Wirawan, Nanda, Akbar, Mahesa

    Published 2018
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  6. 6
    Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM

    Aerofracturelastic on wing box of multi-purpose commuter aircraft under gust lby means of XFEM by Abdullah, Nur Azam, Wirawan, Nanda, Curiel-Sosa, J.L., Akbar, Mahesa

    Published 2018
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  7. 7
    Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure

    Numerical inspection based on Quasi-Static Analysis using Rousselier Damage Model for aluminium wingbox aircraft structure by Ahmad, Meor iqram Meor, Curiel-Sosa, J.L., Akbar, Mahesa L., Abdullah, Nur Azam

    Published 2018
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