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Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects

AIAA journal, 2004-04, Vol.42 (4), p.687-695

2004

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Suppression of Thermal Postbuckling and Nonlinear Panel Flutter Motions Using Piezoelectric Actuators

AIAA journal, 2007-08, Vol.45 (8), p.1861-1873

2007

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Thermal post-buckling and aeroelastic behaviour of shape memory alloy reinforced plates

Smart materials and structures, 2002-04, Vol.11 (2), p.297-307

2002

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Using Aeroelastic Modes for Nonlinear Panel Flutter at Arbitrary Supersonic Yawed Angle

AIAA journal, 2003-02, Vol.41 (2), p.272-279

2003

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Active Control of Nonlinear Panel Flutter Under Yawed Supersonic Flow

AIAA journal, 2005-03, Vol.43 (3), p.671-680

2005

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Adaptive Control of Nonlinear Free Vibrations of Composite Plates Using Piezoelectric Actuators

AIAA journal, 2006-06, Vol.44 (6), p.1169-1180

2006

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Nonlinear Response and Fatigue Life of Isotropic Panels Subjected to Nonwhite Noise

Journal of aircraft, 2006-07, Vol.43 (4), p.975-979

2006

Volltextzugriff (PDF)

Supersonic Nonlinear Panel Flutter Suppression Using Shape Memory Alloys

Journal of aircraft, 2007-07, Vol.44 (4), p.1139-1149

2007

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Finite Element Multiple-Mode Approach to Nonlinear Free Vibrations of Shallow Shells

AIAA journal, 2004-11, Vol.42 (11), p.2373-2381

2004

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Flutter and Thermal Deflection Suppression of Composite Plates Using Shape Memory Alloy

AIAA journal, 2005-09, Vol.43 (9), p.2015-2023

2005

Volltextzugriff (PDF)

Application of aeroelastic modes on nonlinear supersonic panel flutter at elevated temperatures

Computers & structures, 2006-09, Vol.84 (24), p.1619-1628

2006

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Nonlinear Random Response of Panels in an Elevated Thermal-Acoustic Environment

Journal of aircraft, 2003-07, Vol.40 (4), p.683-691

2003

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THERMAL POSTBUCKLING OF COMPOSITE PLATES USING THE FINITE ELEMENT MODAL COORDINATE METHOD

Journal of thermal stresses, 1999-08, Vol.22 (6), p.595-614

Yucheng Shi, Raymond Y. Y. Lee, Chuh Mei

1999

Volltextzugriff (PDF)

Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow

AIAA journal, 1993-01, Vol.31 (1), p.154-162

1993

Volltextzugriff (PDF)

Finite Element Modeling of MFC/AFC Actuators and Performance of MFC

Journal of intelligent material systems and structures, 2001-09, Vol.12 (9), p.601-612

2001

Volltextzugriff (PDF)

Finite element time domain - Modal formulation for nonlinear flutter of composite panels

AIAA journal, 1994-10, Vol.32 (10), p.2044-2052

1994

Volltextzugriff (PDF)

Thermal Buckling Suppression of Supersonic Vehicle Surface Panels Using Shape Memory Alloy

Journal of aircraft, 2004-11, Vol.41 (6), p.1498-1504

2004

Volltextzugriff (PDF)

Flow Angle, Temperature, and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary

Journal of aircraft, 2003-03, Vol.40 (2), p.248-255

2003

Volltextzugriff (PDF)

Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method

AIAA journal, 1995-06, Vol.33 (6), p.1098-1105

1995

Volltextzugriff (PDF)

Finite element analysis of large-amplitude panel flutter of thin laminates

AIAA journal, 1993-04, Vol.31 (4), p.701-707

1993

Volltextzugriff (PDF)

Finite Element Method for Nonlinear Free Vibrations of Composite Plates

AIAA journal, 1997-01, Vol.35 (1), p.159-166

1997

Volltextzugriff (PDF)

Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow

AIAA journal, 1993-06, Vol.31 (6), p.1090-1099

1993

Volltextzugriff (PDF)

Response of plates under statistically unsynchronized uniform random loads using Monte-Carlo simulation

Journal of computational and applied mechanics, 2014, Vol.9 (1), p.3-18

2014

Volltextzugriff (PDF)

Methodology for Supersonic Panel Flutter Analysis of Thermal Protection System Seals

Journal of aircraft, 2001-11, Vol.38 (6), p.1025-1031

2001

Volltextzugriff (PDF)

Finite element model formulation for hypersonic panel flutter analysis with thermal effects

AIAA journal, 2004-04, Vol.42 (4), p.687

2004

Volltextzugriff (PDF)

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Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects

Suppression of Thermal Postbuckling and Nonlinear Panel Flutter Motions Using Piezoelectric Actuators

Thermal post-buckling and aeroelastic behaviour of shape memory alloy reinforced plates

Using Aeroelastic Modes for Nonlinear Panel Flutter at Arbitrary Supersonic Yawed Angle

Active Control of Nonlinear Panel Flutter Under Yawed Supersonic Flow

Adaptive Control of Nonlinear Free Vibrations of Composite Plates Using Piezoelectric Actuators

Nonlinear Response and Fatigue Life of Isotropic Panels Subjected to Nonwhite Noise

Supersonic Nonlinear Panel Flutter Suppression Using Shape Memory Alloys

Finite Element Multiple-Mode Approach to Nonlinear Free Vibrations of Shallow Shells

Flutter and Thermal Deflection Suppression of Composite Plates Using Shape Memory Alloy

Application of aeroelastic modes on nonlinear supersonic panel flutter at elevated temperatures

Nonlinear Random Response of Panels in an Elevated Thermal-Acoustic Environment

THERMAL POSTBUCKLING OF COMPOSITE PLATES USING THE FINITE ELEMENT MODAL COORDINATE METHOD

Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow

Finite Element Modeling of MFC/AFC Actuators and Performance of MFC

Finite element time domain - Modal formulation for nonlinear flutter of composite panels

Thermal Buckling Suppression of Supersonic Vehicle Surface Panels Using Shape Memory Alloy

Flow Angle, Temperature, and Aerodynamic Damping on Supersonic Panel Flutter Stability Boundary

Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method

Finite element analysis of large-amplitude panel flutter of thin laminates

Finite Element Method for Nonlinear Free Vibrations of Composite Plates

Large-Amplitude Finite Element Flutter Analysis of Composite Panels in Hypersonic Flow

Response of plates under statistically unsynchronized uniform random loads using Monte-Carlo simulation

Methodology for Supersonic Panel Flutter Analysis of Thermal Protection System Seals

Finite element model formulation for hypersonic panel flutter analysis with thermal effects

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