All Stories

  1. Nonlinear Dynamic Analyses of STS-1 Forward RCS Oxidizer Tank Structural Failure

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  2. A non-linear Ritz method for progressive failure analysis of variable angle tow composite laminates

    Article • Mechanics of Advanced Materials and Structures, October 2022, Taylor & Francis

    Prof Alberto Milazzo, Dr Vincenzo Oliveri, Dario Campagna

  3. Dynamic analysis of prestressed variable stiffness composite shell structures

    Article • Thin-Walled Structures, June 2022, Elsevier

    Dr Vincenzo Oliveri

  4. Reconfigurable helical lattices via topological morphing

    Article • Materials & Design, August 2021, Elsevier

    Dr Vincenzo Oliveri

  5. Design of a unitized thermoplastic composite out-of-autoclave three-bay wingbox demonstrator

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  6. Continuous Tow Steering around an Elliptical Cut-out in a Composite Panel

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  7. Ritz Solution for Transient Analysis of Variable-Stiffness Shell Structures

    Article • AIAA Journal, April 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri, Prof Alberto Milazzo

  8. Static test of a variable stiffness thermoplastic composite wingbox under shear, bending and torsion

    Article • The Aeronautical Journal, January 2020, Cambridge University Press

    Dr Vincenzo Oliveri

  9. A semi-analytical approach for the analysis of variable-stiffness panels with curvilinear stiffeners

    Article • International Journal of Solids and Structures, October 2019, Elsevier

    Dr Vincenzo Oliveri

  10. Design, Manufacture and Test of an In-Situ Consolidated Thermoplastic Variable-Stiffness Wingbox

    Article • AIAA Journal, April 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri, Robert Telford

  11. Concurrent design and manufacture of a thermoplastic composite stiffener

    Article • Composite Structures, March 2019, Elsevier

    Dr Vincenzo Oliveri

  12. Buckling and post-buckling analysis of cracked stiffened panels via an X-Ritz method

    Article • Aerospace Science and Technology, January 2019, Elsevier

    Prof Alberto Milazzo, Dr Vincenzo Oliveri

  13. A study of the influence of processing parameters on steering of carbon Fibre/PEEK tapes using laser-assisted tape placement

    Article • Composites Part B Engineering, November 2018, Elsevier

    Dr Vincenzo Oliveri

  14. A Rayleigh-Ritz approach for postbuckling analysis of variable angle tow composite stiffened panels

    Article • Computers & Structures, February 2018, Elsevier

    Dr Vincenzo Oliveri

  15. Static Test of a Thermoplastic Composite Wingbox Under Shear and Bending Moment

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  16. Enhanced Buckling Performance of a Stiffened, Variable Angle Tow Thermoplastic Composite Panel

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Robert Telford, Dr Vincenzo Oliveri

  17. Thermoplastic Composite Stiffener Design with Manufacturing Considerations

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  18. Steering of Carbon Fiber/Thermoplastic Pre-preg Tapes using Laser-Assisted Tape Placement

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  19. Design, optimization and manufacturing of a unitized carbon fiber/thermoplastic wingbox structure

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Vincenzo Oliveri

  20. Thermo-mechanical post-buckling analysis of variable angle tow composite plate assemblies

    Article • Composite Structures, January 2018, Elsevier

    Dr Vincenzo Oliveri

  21. Buckling and Postbuckling of Stiffened Composite Panels with Cracks and Delaminations by Ritz Approach

    Article • AIAA Journal, September 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Alberto Milazzo, Dr Vincenzo Oliveri

  22. Post-Buckling Analysis of Damaged Multilayered Composite Stiffened Plates by Rayleigh-Ritz Method

    Article • Applied Mechanics and Materials, March 2016, Trans Tech Publications

    Prof Alberto Milazzo, Dr Vincenzo Oliveri

  23. Post-buckling analysis of cracked multilayered composite plates by pb-2 Rayleigh–Ritz method

    Article • Composite Structures, November 2015, Elsevier

    Prof Alberto Milazzo, Dr Vincenzo Oliveri