Authors Index

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Author	Manuscripts
Pedro Paglione Instituto Tecnológico de Aeronáutica	118 Rayleigh-Ritz method with multibody dynamics for highly flexible structures
Rafael Palacios Imperial College London	29 Modelling complex actuator and sensor architectures for gust alleviation systems of flexible aircraft 28 Effect of gust models on the response prediction of a very flexible wind tunnel wing model 82 Differentiable Aeroelastic Framework Suitable for Industrial Modelling of Nonlinear Loads on Accelerators 137 Nonlinear Gust Effects On Flexible Aircraft With Flared Hinged Wings
Nicola Paletta Airbus Defence and Space	231 Wind tunnel tests for gust load investigation in transonic flows – Part 1 : Development of an innovative test rig
Asa Palmer University of Dayton Research Institute	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Aditya Panigrahi The University of Texas at Austin	185 Experimental Validation of Strain-Load Neural Network Model on a Slender Hypersonic Vehicle
Alexander Pankonien Air Force Research Lab	13 Aeroelastic Wind Tunnel Testing of 3D-Printed Semispan Wings
Younggeun Park Seoul National University	135 Machine learning-based parametric model order reduction for the gust load analysis
Bálint Patarics HUN-REN Institute for Computer Science and Control	99 Flexible aircraft conceptual co-design based on the RCE framework
Mario Peinado Garcia Sapienza University of Rome - Department of Mechanical and Aerospace Engineering	194 Multidisciplinary design optimisation of an aircraft with the semi-aeroelastic hinge device
Alex Pereira do Prado Embraer S. A.	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Amanda Perroni Embraer	159 Wind tunnel flutter test results comparison with computational results of a half-span wing
Luisa Piccolo Serafim Duke University	81 Limit Cycle Oscillation of a Plate with Piezoelectric Elements in Supersonic Flow 16 Exploring the Effect of Different Shock Impingement Angles on Aeroelastic Response for a Thin Panel
Alberto Pirrera University of Bristol	31 Influence of Load Introduction Method on Wingbox Optimization with Nonlinear Structural Stability Constraints
Dale Pitt The Boeing Company - Retired	6 Flutter and Gust Response of a Wing with Aerodynamic Gaps
Marco Pizzoli Sapienza University of Rome	161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics
Antoine Placzek ONERA	162 Towards modular aeroelastic simulations : recent developments and applications at ONERA 150 Influence of aerodynamic modeling on the whirl flutter stability of a propeller under axial and non-axial flow conditions
Charles Poussot-Vassal DTIS, ONERA, Universite de Toulouse, 31000, Toulouse, France	227 Wind Tunnel Tests for Gust Load Investigation in transonic flows – Part 2: Experimental results and control demonstration
Beatriz Pulido Airbus Defence and	171 Feedforward backpropagation artificial neural networks applied to dynamic loads of a military transport aircraft
Luca Pustina Sapienza University of Rome	161 Nonlinear aeroelastic analysis of a regional airliner wing via a neural-network based reduced order model for aerodynamics

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [Q] [R] [S] [T] [V] [W] [X] [Y] [Z]