Flapping Wing CFD/CSD Aeroelastic Formulation Based on a Co-Rotational Shell Finite Element

doi 10.2514/6.2009-2412
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Combined Co-Rotational Beam/Shell Elements for Fluid–structure Interaction Analysis of Insect-Like Flapping Wing

Nonlinear Dynamics
ControlSystems EngineeringMechanical EngineeringElectronic EngineeringApplied MathematicsElectricalOcean EngineeringAerospace Engineering
2019English

Piezoelectric Co-Rotational 3-Node Shell Element

American Journal of Engineering and Applied Sciences
Geotechnical EngineeringEnergy EngineeringEngineering GeologyEngineeringChemical EngineeringPower TechnologyEnvironmental EngineeringComputer Science
2016English

Rotational Invariants in Finite Element Formulation of Three-Dimensional Beam Theories

English

Optical Flow on a Flapping Wing Robot

2009English

A New Finite Element Formulation for Nonlinear Vibration Analysis of the Hard-Coating Cylindrical Shell

Coatings
SurfacesFilmsCoatingsMaterials ChemistryInterfaces
2017English

A Finite Element Formulation Satisfying the Discrete Geometric Conservation Law Based on Averaged Jacobians

International Journal for Numerical Methods in Fluids
Computational MechanicsMechanics of MaterialsApplied MathematicsComputer Science ApplicationsMechanical Engineering
2011English

Finite Element Formulation for Modelling a Frictional Sliding Cable Element

2019English

A Geometrically Non-Linear Piezoelectric Solid Shell Element Based on a Mixed Multi-Field Variational Formulation

International Journal for Numerical Methods in Engineering
Applied MathematicsNumerical AnalysisEngineering
2005English

Recent Developments of a Coupled CFD/CSD Methodology

Lecture Notes in Computer Science
Computer ScienceTheoretical Computer Science
2001English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy