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Numerical simulation and experimental validation of slender wings flutter behaviour

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2019-12, Vol.233 (16), p.5913-5928

2019

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

Composite structures, 2008-04, Vol.83 (2), p.143-153

2008

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Equivalent Material Identification in Composite Scaled Hulls Vertical Impact Tests

Dynamic Response and Failure of Composite Materials, 2023, p.43-50

2023

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

Journal of aerospace engineering, 2014-01, Vol.27 (1), p.112-120

2014

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HALE wing experiments and computational models to predict nonlinear flutter and dynamic response

Aeronautical journal, 2019-06, Vol.123 (1264), p.912-946

2019

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Comparison of numerical analyses of a composite wing component subjected to 4-point bending

Composites. Part C, Open access, 2022-07, Vol.8, p.100264, Article 100264

2022

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Critical behaviour of slender wing configurations

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2010-05, Vol.224 (5), p.587-600

2010

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Design of a High-Altitude Long-Endurance Solar-Powered Unmanned Air Vehicle for Multi-Payload and Operations

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2007-04, Vol.221 (2), p.199-216

2007

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Structural Uncertainty Effect on Classical Wing Flutter Characteristics

Journal of aerospace engineering, 2010-10, Vol.23 (4), p.327-338

2010

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Aeroelastic behaviour of a solar-powered high-altitude long endurance unmanned air vehicle (HALE-UAV) slender wing

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2004-06, Vol.218 (3), p.179-188

Frulla, G

2004

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A Practical Engineering Approach to the Design and Manufacturing of a mini kW BladeWind Turbine: Definition, optimization and CFD Analysis

Fluid dynamics & materials processing, 2015-01, Vol.11 (3), p.257-277

2015

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Preliminary reliability design of a solar-powered high-altitude very long endurance unmanned air vehicle

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2002-01, Vol.216 (4), p.189-196

Frulla, G

2002

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Heliplat®: high altitude very-long endurance solar powered UAV for telecommunication and Earth observation applications

Aeronautical journal, 2004-06, Vol.108 (1084), p.277-293

2004

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

Journal of aircraft, 2004-11, Vol.41 (6), p.1505-1520

2004

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Experimental Determination of Aeroelastic Derivatives for a Small-Scale Bridge Deck

International Journal of Mechanics, 2018, Vol.12, p.67-78

2018

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Nonlinear LCO “amplitude–frequency” characteristics for plates fluttering at supersonic speeds

International journal of non-linear mechanics, 2015-12, Vol.77, p.51-60

2015

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Rigid rotor dynamic stability using Floquet theory

European journal of mechanics, A, Solids, 2000, Vol.19 (1), p.139-150

Frulla, Giacomo

2000

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

Journal of composite materials, 1995-04, Vol.29 (6), p.751-765

1995

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

International journal of non-linear mechanics, 1997-11, Vol.32 (6), p.1017-1033

1997

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Cicala's asymptotic approach to the linear shell theory

Composite structures, 2001-04, Vol.52 (1), p.13-26

2001

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

Modern physics letters. B, Condensed matter physics, statistical physics, applied physics, 1991-12, Vol.5 (29), p.1911-1918

1991

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

International journal of solids and structures, 1994-03, Vol.31 (6), p.763-783

1994

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

Journal of aircraft, 1995-11, Vol.32 (6), p.1375-1381

1995

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

Journal of aircraft, 1994-11, Vol.31 (6), p.1297-1302

1994

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A New Test Facility for Measuring the Coefficient of Moisture Expansion of Advanced Composite Materials

Journal of composites technology & research, 1992-12, Vol.14 (4), p.225

1992

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Numerical simulation and experimental validation of slender wings flutter behaviour

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

Equivalent Material Identification in Composite Scaled Hulls Vertical Impact Tests

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

HALE wing experiments and computational models to predict nonlinear flutter and dynamic response

Comparison of numerical analyses of a composite wing component subjected to 4-point bending

Critical behaviour of slender wing configurations

Design of a High-Altitude Long-Endurance Solar-Powered Unmanned Air Vehicle for Multi-Payload and Operations

Structural Uncertainty Effect on Classical Wing Flutter Characteristics

Aeroelastic behaviour of a solar-powered high-altitude long endurance unmanned air vehicle (HALE-UAV) slender wing

A Practical Engineering Approach to the Design and Manufacturing of a mini kW BladeWind Turbine: Definition, optimization and CFD Analysis

Preliminary reliability design of a solar-powered high-altitude very long endurance unmanned air vehicle

Heliplat®: high altitude very-long endurance solar powered UAV for telecommunication and Earth observation applications

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

Experimental Determination of Aeroelastic Derivatives for a Small-Scale Bridge Deck

Nonlinear LCO “amplitude–frequency” characteristics for plates fluttering at supersonic speeds

Rigid rotor dynamic stability using Floquet theory

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

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

Cicala's asymptotic approach to the linear shell theory

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

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

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

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

A New Test Facility for Measuring the Coefficient of Moisture Expansion of Advanced Composite Materials

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