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Cestino, Enrico

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Aerospace (7)

Topics

Wings (6) Aerodynamics (4) Scale models (3) Aircraft (2) Composite materials (2) Mathematical models (2) Optimization (2) Wind tunnel tests (2) Adaptive control (1) Architecture (1) Business and general aviation aircraft (1) Calibration (1) Electric aircraft (1) Electric motors (1) Flight tests (1) Fuel cells (1) Gases (1) Manufacturing processes (1) Parts (1) Propellers and rotors (1) Simulation and modeling (1) Stall (1) Starters and starting (1) Tools and equipment (1) Unmanned aerial vehicles (1) Vehicle dynamics /flight dynamics (1) Wind power (1)

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Cestino, Enrico (11) Frulla, Giacomo (8) Marzocca, Piergiovanni (6) Arias-Montano, Alfredo (1) Baghdasaryan, Gevorg (1) Battipede, Manuela (1) Behal, Aman (1) Borello, Fabio (1) Bruni, Claudia (1) Carrese, Robert (1) Cassaro, Mario (1) Correa, Gabriel (1) Cravana, Andrea (1) Danzi, Francesco (1) Duella, Renzo (1) Gati, Balazs (1) Gili, Piero (1) Manfreda, Gerardo (1) Mikilyan, Marine (1) Nagy, Andras (1)

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SAE (11)

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Politecnico di Torino (11) Clarkson University (3) RMIT University (2) Blue Engineering SRL (1) Budapest University of Technology & Economics (1) Clarkson Univ (1) Institute of Mechanics (1) Instituto Politecnico Nacional, ESIME-IP (1) Tescogo SPA (1) University of Central Florida (1)

Events

SAE 2013 AeroTech Congress & Exhibition (4) AeroTech Congress & Exhibition (3) Aerospace Technology Conference and Exposition (2) SAE 2015 AeroTech Congress & Exhibition (2)

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Select Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings

Nonlinear Slender Beam-Wise Schemes for Structural Behavior of Flexible UAS Wings

Technical Paper
2015-01-2462
DOI: https://doi.org/10.4271/2015-01-2462

Published 2015-09-15 by SAE International in United States

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Select Improved Multibody Model of Flexible Wing

Improved Multibody Model of Flexible Wing

Technical Paper
2013-01-2265
DOI: https://doi.org/10.4271/2013-01-2265

Published 2013-09-17 by SAE International in United States

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

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

Technical Paper
2013-01-2160
DOI: https://doi.org/10.4271/2013-01-2160

Published 2013-09-17 by SAE International in United States

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Select Efficient Procedure for Robust Optimal Design of Aerospace Laminated Structures

Efficient Procedure for Robust Optimal Design of Aerospace Laminated Structures

Technical Paper
2017-01-2058
DOI: https://doi.org/10.4271/2017-01-2058

Published 2017-09-19 by SAE International in United States

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Select Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams

Application of Structural Topology Optimization to Couple Thin-Walled Stiffened Box-Beams

Technical Paper
2017-01-2059
DOI: https://doi.org/10.4271/2017-01-2059

Published 2017-09-19 by SAE International in United States

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Select Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems

Aeroelastic Behaviour of Flexible Wings Carrying Distributed Electric Propulsion Systems

Technical Paper
2017-01-2061
DOI: https://doi.org/10.4271/2017-01-2061

Published 2017-09-19 by SAE International in United States

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Select A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings

A Reduced Order Model for the Aeroelastic Analysis of Flexible Wings

SAE International Journal of Aerospace

Journal Article
2013-01-2158

Published 2013-09-17 by SAE International in United States

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Select ℒ ₁ Adaptive Flutter Suppression Control Strategy for Highly Flexible Structure

ℒ ₁ Adaptive Flutter Suppression Control Strategy for Highly Flexible Structure

SAE International Journal of Aerospace

Journal Article
2013-01-2263

Published 2013-09-17 by SAE International in United States

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Select A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience

A Fuel Cell Based Propulsion System for General Aviation Aircraft: The ENFICA-FC Experience

SAE International Journal of Aerospace

Journal Article
2011-01-2522

Published 2011-10-18 by SAE International in United States

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Select Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings

Theoretical and Experimental Flutter Predictions in High Aspect Ratio Composite Wings

SAE International Journal of Aerospace

Journal Article
2011-01-2722

Published 2011-10-18 by SAE International in United States

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