ALPES publications

A Doublet-Lattice Method Correction Approach for High Fidelity Gust Loads Analysis
Valente C et al., 2017, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2017-0632
An optimized doublet-lattice method correction approach for a large civil aircraft
Valente C et al., 2017, International Forum on Aeroelasticity and Structural Dynamics (IFASD)
Frequency Domain Approach for Transonic Aerodynamic Modelling Applied to a Viscous Wing
Poncet-Montanges A et al., 2017, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2017-0075
Nonlinear negative stiffness wing-tip spring device for gust loads alleviation
Castrichini A et al., 2017, 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-1574
Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation
Castrichini A et al., Mar 2017, In: Journal of Aircraft, vol 54, no 2 10.2514/1.C033887
Nonlinear Static Aeroelasticity of High Aspect Ratio Wing Aircraft by FEM and Multibody Methods
Castellani M et al., Mar 2017, In: Journal of Aircraft, vol 54, no 2 10.2514/1.C033825
Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation
Castrichini A et al., Jan 2017, In: Aeronautical Journal, vol 121, no 1235 10.1017/aer.2016.108
Aircraft Loads Prediction Using Enhanced Simulation (ALPES)
Cooper J et al., 2016, 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-1571
Bifurcation Analysis of a Nose Landing Gear System
Tartaruga I et al., 2016, 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-1572
Doublet-Lattice Method Correction by Means of Linearised Frequency Domain Solver Analysis
Valente C et al., 2016, 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-1575
Flight Loads Prediction of High Aspect Ratio Wing Aircraft using Multibody Dynamics
Castellani M et al., 27 Dec 2016, In: SAE International Journal of Aerospace, vol 2016 10.1155/2016/4805817
Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling
Poncet-Montanges A et al., 2016, 15th Dynamics Specialists Conference, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-1576
Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling applied to a 3D Wing
Poncet-Montanges A et al., 2016, AIAA Modeling and Simulation Technologies Conference, 2016, American Institute of Aeronautics and Astronautics Inc. (AIAA) 10.2514/6.2016-4010
Openfsi interface for strongly coupled steady and unsteady aeroelasticity
Valente C et al., 2016, International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015, International Forum on Aeroelasticity and Structural Dynamics (IFASD)
Parametric reduced order model approach for rapid dynamic loads prediction
Castellani M et al., May 2016, In: Aerospace Science and Technology, vol 52 10.1016/j.ast.2016.02.015
Parametric reduced-order model approach for simulation and optimization of aeroelastic systems with structural nonlinearities
Castellani M et al., Jun 2016, In: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol 230, no 8 10.1177/0954410015608888
Prediction and uncertainty propagation of correlated time-varying quantities using surrogate models
Tartaruga I et al., 1 Mar 2016, In: CEAS Aeronautical Journal, vol 7, no 1 10.1007/s13272-015-0172-1
Efficient Prediction and Uncertainty Propagation of Correlated Loads
Tartaruga I et al., 9 Jan 2015 10.2514/6.2015-1847
Frequency-domain approach for transonic unsteady aerodynamics modelling
Poncet-Montanges A et al., 2015, International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015, International Forum on Aeroelasticity and Structural Dynamics (IFASD)
Nonlinear Folding Wing-Tips for Gust Loads Alleviation
Castrichini A et al., 30 Nov 2015 10.2514/6.2015-1846
Reduced Order Model Approach for Efficient Aircraft Loads Prediction
Castellani M et al., Dec 2015, In: SAE International Journal of Aerospace, vol 8, no 2 10.4271/2015-01-2568