Zhen et al., 2023 - Google Patents
Aeroelastic analysis and active control of one-dimensional acoustic black hole structures in supersonic airflowZhen et al., 2023
- Document ID
- 2051369265797688349
- Author
- Zhen Y
- Gu T
- Tang Y
- Publication year
- Publication venue
- Engineering Analysis with Boundary Elements
External Links
Snippet
In this paper, the aeroelastic characteristic and active control of one-dimensional acoustic black hole structures in supersonic airflow are analyzed. Utilizing Hamilton's principle, the equation of motion of the one-dimensional acoustic black hole (ABH) structures in …
- 238000004458 analytical method 0 title description 25
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Zhen et al. | Aeroelastic analysis and active control of one-dimensional acoustic black hole structures in supersonic airflow | |
Kolahchi et al. | Visco-nonlocal-refined Zigzag theories for dynamic buckling of laminated nanoplates using differential cubature-Bolotin methods | |
Luo et al. | Dynamics of delaminated beams | |
Zhang et al. | Vibro-acoustic analysis of the thin laminated rectangular plate-cavity coupling system | |
Song et al. | Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate | |
Carrera et al. | Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications | |
Qiu et al. | Optimal placement and active vibration control for piezoelectric smart flexible cantilever plate | |
AkhavanAlavi et al. | Active control of micro Reddy beam integrated with functionally graded nanocomposite sensor and actuator based on linear quadratic regulator method | |
Wang | On buckling of column structures with a pair of piezoelectric layers | |
Kazancı | Dynamic response of composite sandwich plates subjected to time-dependent pressure pulses | |
Lu et al. | Vibration suppression of cantilevered piezoelectric laminated composite rectangular plate subjected to aerodynamic force in hygrothermal environment | |
Song et al. | Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow | |
Guo et al. | Modeling and analyze of behaviors of functionally graded graphene reinforced composite beam with geometric imperfection in multiphysics | |
Zhang et al. | A lattice sandwich structure with the active variable stiffness device under aerodynamical condition | |
Chai et al. | Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries | |
Nayak et al. | Process for design optimization of honeycomb core sandwich panels for blast load mitigation | |
Sankar et al. | Panel flutter characteristics of sandwich plates with CNT reinforced facesheets using an accurate higher-order theory | |
Song et al. | Dynamic responses of aerothermoelastic functionally graded CNT reinforced composite panels in supersonic airflow subjected to low-velocity impact | |
Nguyen-Thoi et al. | Analysis and optimal control of smart damping for porous functionally graded magneto-electro-elastic plate using smoothed FEM and metaheuristic algorithm | |
Hong | Thermal vibration and transient response of magnetostrictive functionally graded material plates | |
Bayat et al. | Analytical solution for free vibration of laminated curved beam with magnetostrictive layers | |
Miao et al. | Closed-form solution considering the tangential effect under harmonic line load for an infinite Euler–Bernoulli beam on elastic foundation | |
Muc et al. | Free vibrations and supersonic flutter of multilayered laminated cylindrical panels | |
An et al. | Nonlinear aeroelastic analysis of curved laminated composite panels | |
Liu et al. | Free and forced vibration analysis of pyramid lattice sandwich plate based on the dimensional reduction model |