All Stories

  1. Uncertainty Quantification of High-Velocity Impact Fracture in Fiber-Reinforced Composites Using a Robust Stochastic Sampling Approach.

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

    Dr Giacomo Frulla

  2. Aeroelastic Analysis through Non-Linear Beam Finite Elements with Bending-Torsion Coupling Formulation

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

    Dr Giacomo Frulla

  3. Numerical simulation and experimental validation of slender wings flutter behaviour

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, October 2019, SAGE Publications

    Dr Giacomo Frulla

  4. An invariant-based performance-oriented procedure for preliminary design of composite structures

    Article • Aircraft Engineering and Aerospace Technology, April 2018, Emerald

    Dr Giacomo Frulla

  5. MDO/MSO of Slender Thin Walled Box Beam Model

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla, Francesco Danzi

  6. Design, Analysis and Experimental Testing of a Morphing Wing

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla, Mr Joan Marc Martinez

  7. Parametric analysis of a fluttering piezoelectric wing

    Article • Aircraft Engineering and Aerospace Technology, May 2016, Emerald

    Dr Giacomo Frulla

  8. Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment

    Article • Aircraft Engineering and Aerospace Technology, March 2015, Emerald

    Dr Giacomo Frulla

  9. A Multi-Objective Nonlinear Piezoaeroelastic Wing Solution for Energy Harvesting and Load Alleviation: Modeling and Simulation

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  10. Development of an Aeroelastic Wing Model With Piezoelectric Elements for Gust Load Alleviation and Energy Harvesting

    Article • November 2014, ASME International

    Dr Giacomo Frulla

  11. Analysis of slender thin-walled anisotropic box-beams including local stiffness and coupling effects

    Article • Aircraft Engineering and Aerospace Technology, July 2014, Emerald

    Dr Giacomo Frulla

  12. Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws

    Article • Journal of Aerospace Engineering, January 2014, American Society of Civil Engineers (ASCE)

    Dr Giacomo Frulla

  13. Static/Fatigue Structural Behaviour of Damaged Stiffened Composite Plates for UAS Applications

    Article • September 2013, SAE International

    Dr Giacomo Frulla

  14. A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings

    Article • SAE International Journal of Aerospace, September 2013, SAE International

    Dr Giacomo Frulla

  15. The Influence of Supersonic Stream on the Dependence "Amplitude-Frequency" of Nonlinear Vibrations of Flexible Plate

    Article • September 2013, SAE International

    Dr Giacomo Frulla

  16. WindDesigner: An open tool for analysis and design of wind generators

    Article • June 2013, Institute of Electrical & Electronics Engineers (IEEE)

    Dr Giacomo Frulla

  17. Safety Assessment of Pharmaceutical Distribution in a Hospital Environment

    Article • Journal of Healthcare Technology and Management, January 2013, Columbia International Publishing

    Dr Giacomo Frulla

  18. Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings

    Article • SAE International Journal of Aerospace, October 2011, SAE International

    Dr Giacomo Frulla

  19. Structural Uncertainty Effect on Classical Wing Flutter Characteristics

    Article • Journal of Aerospace Engineering, October 2010, American Society of Civil Engineers (ASCE)

    Dr Giacomo Frulla

  20. Research Activities on Buckling of Composite Structures in Italy

    Article • May 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  21. Numerical/experimental structural characterization of composite advanced joints for HALE-UAV platforms

    Article • Composites Part B Engineering, June 2008, Elsevier

    Dr Giacomo Frulla

  22. Design, manufacturing and testing of a HALE-UAV structural demonstrator

    Article • Composite Structures, April 2008, Elsevier

    Dr Giacomo Frulla

  23. Stability and Control of a High-Altitude, Long-Endurance UAV

    Article • Journal of Guidance Control and Dynamics, May 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  24. Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs

    Article • May 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  25. Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings

    Article • May 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  26. HELIPLAT: Design, Aerodynamic, Structural Analysis of Long- Endurance Solar-Powered Stratospheric Platform

    Article • Journal of Aircraft, November 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  27. HELIPLAT: Aerodynamic and Structural Analysis of HAVE Solar Powered Platform.

    Article • May 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  28. Cicala's asymptotic approach to the linear shell theory

    Article • Composite Structures, April 2001, Elsevier

    Dr Giacomo Frulla

  29. Rigid rotor dynamic stability using Floquet theory

    Article • European Journal of Mechanics - A/Solids, January 2000, Elsevier

    Dr Giacomo Frulla

  30. Post-buckling behaviour of graphite/epoxy stiffened panels with initial imperfections subjected to eccentric biaxial compression loading

    Article • International Journal of Non-Linear Mechanics, November 1997, Elsevier

    Dr Giacomo Frulla

  31. Nonlinear analysis of graphite epoxy/wing boxes under pure bending including lateral pressure

    Article • Journal of Aircraft, November 1995, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  32. Analytical and Experimental Results of the Coefficient of Thermal Expansion of High-Modulus Graphite-Epoxy Materials

    Article • Journal of Composite Materials, April 1995, SAGE Publications

    Dr Giacomo Frulla

  33. Nonlinear angle of twist of advanced composite wing boxes under pure torsion

    Article • Journal of Aircraft, November 1994, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Giacomo Frulla

  34. Nonlinear analysis of anisotropic plates with initial imperfections and various boundary conditions subjected to combined biaxial compression and shear loads

    Article • International Journal of Solids and Structures, March 1994, Elsevier

    Dr Giacomo Frulla

  35. STRETCHED EXPONENTIAL STRUCTURAL RELAXATION OF COMPOSITE MATERIALS INDUCED BY IMPURITIES DESORPTION IN VACUUM

    Article • Modern Physics Letters B, December 1991, World Scientific Pub Co Pte Lt

    Dr Giacomo Frulla