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Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1370
Published Online: January 23, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Editorial
J. Vib. Acoust.
Paper No: VIB-23-1016
Published Online: January 23, 2023
Topics:
Acoustic emissions
Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1302
Published Online: January 11, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1298
Published Online: January 10, 2023
Journal Articles
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust. June 2023, 145(3): 031002.
Paper No: VIB-22-1111
Published Online: January 5, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1272
Published Online: January 5, 2023
Journal Articles
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1314
Published Online: January 5, 2023
Journal Articles
Acoustic radiation from stiffened double concentric large cylindrical shells: Part II Creeping waves
Accepted Manuscript
Journal:
Journal of Vibration and Acoustics
Article Type: Research Papers
J. Vib. Acoust.
Paper No: VIB-22-1315
Published Online: January 5, 2023
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 1 Schematic of a nonlinear cantilever beam with an intermediate concentrated mass deflecting due to distributed pressure from an axial supersonic flow More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 2 Discontinuous rise in flutter Mach number as a concentrated mass ratio η is varied for s η = 0.9 (solid line). If the mass ratio was instead increased in a homogeneous fashion (increasing thickness, dashed line), an abrupt flutter mode switch does not occur. More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 3 Eigenvalue behavior two different concentrated mass ratios: one prior to the discontinuous jump in flutter Mach number (a,b; η = 0.2), and one after (c,d; η = 0.3). For both cases, s η = 0.9 . More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 4 Flutter Mach number behavior as a mass ( η = 0.5) is varied along the length of the plate. From left to right in ( a ), we see in ( b ) that traditional modes 1 and 2 merging drives flutter. At about s η = 0.35 flutter is due to merging of modes 2 and 3 ( c ). Between the dash... More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 5 Purely structural nonlinear behavior when base excited: ( a ) Effect of various nonlinearities on the response of a cantilever plate with no concentrated mass and forcing amplitude F a = 0.075 and ( b ) Effect of several different masses on the nonlinear inertial response with stiffnes... More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 6 LCO properties as dynamic pressure is varied: ( a ) LCO amplitudes as various nonlinear forces are included and ( b ) Corresponding LCO frequencies. Results are for M ∞ = 4 and no point mass. In ( b ), the dotted “Flutter” line indicates the linear flutter frequency. More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 7 LCO amplitudes: ( a ) and LCO frequencies ( b ) as dynamic pressure (Λ) is varied for η = 0.1 and s η = 0.9 More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 8 LCO amplitudes: ( a ) and LCO frequencies ( b ) as mass ratio η is varied (modes 1:2 merging, s η = 0.9 , Λ = 120 ) More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 9 LCO amplitudes: ( a ) and corresponding LCO frequencies and ( b ) for several different mass ratios (modes 1:2 merging, M ∞ = 3, s η = 1 ) More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 10 LCO amplitude hump mode and the effect of varying Mach number (modes 1:2 merging, η = 0.1, s η = 1 ) More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 11 Flutter mode shapes when the flutter mechanism is due to modes 1:2 merging (blue line), modes 2:3 merging (red line), and modes 3:4 merging (green line) (Color version online.) More
Image
in On the Influence of Nonlinear Inertial Forces on the Limit Cycle Oscillations of an Inextensible Plate in a Supersonic Axial Flow
> Journal of Vibration and Acoustics
Published Online: January 5, 2023
Fig. 12 LCO amplitudes: ( a ) and LCO frequencies and ( b ) as dynamic pressure Λ is varied when flutter mechanism is due to modes 2:3 merging ( η = 0.5, s η = 0.7 , 6 modes). FOPT stands for First-Order Piston Theory aerodynamics only. More