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Journal Articles

On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow

Samuel C. Stanton, Sung J. Choi, Kevin A. McHugh

J. Vib. Acoust. June 2023, 145(3): 031002.

Paper No: VIB-22-1111

DOI: https://doi.org/10.1115/1.4056127

Published Online: January 5, 2023

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Topics: Aerodynamics, Axial flow, Flutter (Aerodynamics), Limit cycles, Mach number, Oscillations, Pistons, Pressure, Aeroelasticity, Structural dynamics

Journal Articles

Pseudospectral Continuation for Aeroelastic Stability Analysis

Arion Pons

J. Vib. Acoust. August 2022, 144(4): 044501.

Paper No: VIB-22-1027

DOI: https://doi.org/10.1115/1.4053961

Published Online: March 11, 2022

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Topics: Flutter (Aerodynamics), Stability, Wings, Damping, Flight

Journal Articles

Damage-Mitigating Predictive Control of Airfoil Flutter for a General Hypersonic Flight Vehicle

Xiaohui Zhang, Yuhui Wang, Xingkai Feng, Siyuan Hou

J. Vib. Acoust. October 2019, 141(5): 051007.

Paper No: VIB-18-1323

DOI: https://doi.org/10.1115/1.4043511

Published Online: June 5, 2019

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Topics: Airfoils, Damage, Flutter (Aerodynamics), Predictive control, Control equipment, Flight, Vehicles

Journal Articles

Micropower Generation Using Cross-Flow Instabilities: A Review of the Literature and Its Implications

Mohammed F. Daqaq, Amin Bibo, Imran Akhtar, Ali H. Alhadidi, Meghashyam Panyam, Benjamin Caldwell, Jamie Noel

J. Vib. Acoust. June 2019, 141(3): 030801.

Paper No: VIB-18-1199

DOI: https://doi.org/10.1115/1.4042521

Published Online: February 13, 2019

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Topics: Flow (Dynamics), Generators, Wakes, Flutter (Aerodynamics), Vortex-induced vibration, Design, Oscillations

Journal Articles

Versatile Absolute Nodal Coordinate Formulation Model for Dynamic Folding Wing Deployment and Flutter Analyses

Keisuke Otsuka, Yinan Wang, Kanjuro Makihara

J. Vib. Acoust. February 2019, 141(1): 011014.

Paper No: VIB-18-1087

DOI: https://doi.org/10.1115/1.4041022

Published Online: September 10, 2018

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Topics: Flutter (Aerodynamics), Simulation, Wings, Aerodynamics

Journal Articles

A Method of Panel Flutter Suppression and Elimination for Aeroelastic Structures in Supersonic Airflow

Zhi-Guang Song, Tian-Zhi Yang, Feng-Ming Li, Erasmo Carrera, Peter Hagedorn

J. Vib. Acoust. December 2018, 140(6): 064501.

Paper No: VIB-17-1524

DOI: https://doi.org/10.1115/1.4039724

Published Online: May 7, 2018

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Topics: Air flow, Flutter (Aerodynamics), Stiffness, Pressure, Piezoelectric materials

Journal Articles

Flutter Limit Investigation for a Horizontal Axis Wind Turbine Blade

Mennatullah M. Abdel Hafeez, Ayman A. El-Badawy

J. Vib. Acoust. August 2018, 140(4): 041014.

Paper No: VIB-17-1193

DOI: https://doi.org/10.1115/1.4039402

Published Online: March 27, 2018

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Topics: Blades, Flutter (Aerodynamics), Rotors, Shear (Mechanics), Stability, Wind velocity, Horizontal axis wind turbines, Equations of motion, Finite element methods, Modal analysis

Journal Articles

Analysis of Curved Panel Flutter in Supersonic and Transonic Airflows Using a Fluid–Structure Coupling Algorithm

Guanhua Mei, Jiazhong Zhang, Can Kang

J. Vib. Acoust. August 2017, 139(4): 041004.

Paper No: VIB-16-1105

DOI: https://doi.org/10.1115/1.4036103

Published Online: May 30, 2017

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Topics: Air flow, Algorithms, Deflection, Deformation, Fluids, Flutter (Aerodynamics), Pressure, Stress, Oscillations

Journal Articles

Fuzzy Approximation by a Novel Levenberg–Marquardt Method for Two-Degree-of-Freedom Hypersonic Flutter Model

Y. H. Wang, L. Zhu, Q. X. Wu, C. S. Jiang

J. Vib. Acoust. August 2014, 136(4): 044502.

Paper No: VIB-13-1103

DOI: https://doi.org/10.1115/1.4027524

Published Online: May 19, 2014

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Topics: Airfoils, Approximation, Flutter (Aerodynamics), Errors

Journal Articles

Analysis of Supersonic and Transonic Panel Flutter Using a Fluid-Structure Coupling Algorithm

Guanhua Mei, Jiazhong Zhang, Guang Xi, Xu Sun, Jiahui Chen

J. Vib. Acoust. June 2014, 136(3): 031013.

Paper No: VIB-13-1099

DOI: https://doi.org/10.1115/1.4027135

Published Online: April 3, 2014

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Topics: Air flow, Algorithms, Deformation, Finite element methods, Flow (Dynamics), Fluids, Flutter (Aerodynamics), Oscillations, Pressure, Stress

Journal Articles

Numerical Investigation of the Flutter of a Spherical Shell

Mohamed Menaa, Aouni A. Lakis

J. Vib. Acoust. April 2014, 136(2): 021010.

Paper No: VIB-13-1190

DOI: https://doi.org/10.1115/1.4025997

Published Online: December 24, 2013

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Topics: Flutter (Aerodynamics), Pressure, Shells, Spherical shells, Stiffness

Journal Articles

Efficient Hybrid Finite Element Method for Flutter Prediction of Functionally Graded Cylindrical Shells

Farhad Sabri, Aouni A. Lakis

J. Vib. Acoust. February 2014, 136(1): 011002.

Paper No: VIB-10-1286

DOI: https://doi.org/10.1115/1.4025397

Published Online: September 27, 2013

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Topics: Finite element methods, Flutter (Aerodynamics), Pipes, Shells, Stiffness, Pressure, Materials properties, Ceramics, Functionally graded materials, Modeling

Journal Articles

Three-Dimensional Tailored Vibration Response and Flutter Control of High-Bypass Shroudless Aeroengine Fans

O. G. McGee III, C. Fang

J. Vib. Acoust. April 2013, 135(2): 021010.

Paper No: VIB-09-1001

DOI: https://doi.org/10.1115/1.4006758

Published Online: March 18, 2013

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Topics: Blades, Composite materials, Design, Flutter (Aerodynamics), Stiffness, Fans, Vibration, Polynomials, Optimization, Stress

Journal Articles

Aeroelastic Analysis of Membrane Microair Vehicles—Part I: Flutter and Limit Cycle Analysis for Fixed-Wing Configurations

Peter J. Attar, Raymond E. Gordnier, Jordan W. Johnston, William A. Romberg, Ramkumar N. Parthasarathy

J. Vib. Acoust. April 2011, 133(2): 021008.

DOI: https://doi.org/10.1115/1.4002129

Published Online: March 17, 2011

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Topics: Flow (Dynamics), Flutter (Aerodynamics), Limit cycles, Membranes, Vehicles, Wings, Computation, Oscillations

Journal Articles

Modeling and Testing of a Novel Aeroelastic Flutter Energy Harvester

Matthew Bryant, Ephrahim Garcia

J. Vib. Acoust. February 2011, 133(1): 011010.

DOI: https://doi.org/10.1115/1.4002788

Published Online: January 26, 2011

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Topics: Aerodynamics, Deflection, Energy harvesting, Flutter (Aerodynamics), Limit cycles, Wind velocity, Modeling, Fluid-dynamic forces, Flow (Dynamics), Vibration

Journal Articles

Modeling and Analysis of Piezoelectric Energy Harvesting From Aeroelastic Vibrations Using the Doublet-Lattice Method

Carlos De Marqui, Jr., Wander G. R. Vieira, Alper Erturk, Daniel J. Inman

J. Vib. Acoust. February 2011, 133(1): 011003.

DOI: https://doi.org/10.1115/1.4002785

Published Online: December 8, 2010

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Topics: Air flow, Circuits, Damping, Energy harvesting, Flutter (Aerodynamics), Piezoelectric ceramics, Stress, Vibration, Wings, Excitation

Journal Articles

Effect of Boundary Conditions on Nonlinear Vibration and Flutter of Laminated Cylindrical Shells

E. L. Jansen

J. Vib. Acoust. February 2008, 130(1): 011003.

DOI: https://doi.org/10.1115/1.2775512

Published Online: November 12, 2007

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Topics: Boundary-value problems, Flutter (Aerodynamics), Nonlinear vibration, Pipes, Shells, Stress, Vibration, Buckling, Supersonic flow, Lamination

Journal Articles

Lateral Vibration of Two Axially Translating Beams Interconnected by a Winkler Foundation

Mohamed Gaith, Sinan Müftü

J. Vib. Acoust. June 2007, 129(3): 380–385.

DOI: https://doi.org/10.1115/1.2732353

Published Online: September 13, 2006

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Topics: Mode shapes, Stiffness, Tension, Vibration, Stability, Flutter (Aerodynamics)

Journal Articles

Panel Flutter Model Identification Using the Minimum Model Error Method on the Forced Response Measurements

Oleg V. Shiryayev, Joseph C. Slater

J. Vib. Acoust. October 2006, 128(5): 635–645.

DOI: https://doi.org/10.1115/1.2202160

Published Online: February 8, 2006

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Topics: Errors, Flow (Dynamics), Flutter (Aerodynamics), Transients (Dynamics), Noise (Sound), Response surface methodology, System identification, Eigenvalues, Algorithms, Simulation

Journal Articles

Analysis of Nonlinear Aeroelastic Panel Response Using Proper Orthogonal Decomposition

Sean A. Mortara, Graduate Research Assistant, Joseph Slater, Associate Professor, Philip Beran, Senior Research Aerospace Engineer

J. Vib. Acoust. July 2004, 126(3): 416–421.

DOI: https://doi.org/10.1115/1.1687389

Published Online: July 30, 2004

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Topics: Flutter (Aerodynamics), Principal component analysis, Stability, Differential equations, Degrees of freedom

Journal citation

NARROW

On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow

Pseudospectral Continuation for Aeroelastic Stability Analysis

Damage-Mitigating Predictive Control of Airfoil Flutter for a General Hypersonic Flight Vehicle

Micropower Generation Using Cross-Flow Instabilities: A Review of the Literature and Its Implications

Versatile Absolute Nodal Coordinate Formulation Model for Dynamic Folding Wing Deployment and Flutter Analyses

A Method of Panel Flutter Suppression and Elimination for Aeroelastic Structures in Supersonic Airflow

Flutter Limit Investigation for a Horizontal Axis Wind Turbine Blade

Analysis of Curved Panel Flutter in Supersonic and Transonic Airflows Using a Fluid–Structure Coupling Algorithm

Fuzzy Approximation by a Novel Levenberg–Marquardt Method for Two-Degree-of-Freedom Hypersonic Flutter Model

Analysis of Supersonic and Transonic Panel Flutter Using a Fluid-Structure Coupling Algorithm

Numerical Investigation of the Flutter of a Spherical Shell

Efficient Hybrid Finite Element Method for Flutter Prediction of Functionally Graded Cylindrical Shells

Three-Dimensional Tailored Vibration Response and Flutter Control of High-Bypass Shroudless Aeroengine Fans

Aeroelastic Analysis of Membrane Microair Vehicles—Part I: Flutter and Limit Cycle Analysis for Fixed-Wing Configurations

Modeling and Testing of a Novel Aeroelastic Flutter Energy Harvester

Modeling and Analysis of Piezoelectric Energy Harvesting From Aeroelastic Vibrations Using the Doublet-Lattice Method

Effect of Boundary Conditions on Nonlinear Vibration and Flutter of Laminated Cylindrical Shells

Lateral Vibration of Two Axially Translating Beams Interconnected by a Winkler Foundation

Panel Flutter Model Identification Using the Minimum Model Error Method on the Forced Response Measurements

Analysis of Nonlinear Aeroelastic Panel Response Using Proper Orthogonal Decomposition

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