Books on the topic 'Vibration of circular plate'

Lakis, A. A. Hybrid finite element analysis of circular and annular plates. Dept. of Mechanical Engineering, École polytechnique de Montréal, Campus de l'Université de Montréal, 1995.

Smith, Ralph C. A Galerkin method for linear PDE systems in circular geometries with structural acoustic applications. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Institute for Computer Applications in Science and Engineering., ed. A Galerkin method for linear PDE systems in circular geometries with structural acoustic applications. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Lucio, Maestrello, Bayliss Alvin, and Langley Research Center, eds. Coupling between plate vibration and acoustic radiation. National Aeronautics and Space Administration, Langley Research Center, 1992.

P, Townsend Dennis, Coy John J, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structure. National Aeronautics and Space Administration, 1992.

E, Kielb Robert, ed. Joint research effort on vibrations of twisted plates: Phase 1, final results. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

H, Williams James. Modes of vibration on square fiberglass epoxy composite thick plate. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

C, Marques Elizabeth R., Lee Samson S, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Massachusetts Institute of Technology, and Lewis Research Center, eds. Modes of vibration on square fiberglass epoxy composite thick plate. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Xiang, Y. Plate vibration with arbitrarily oriented stiffeners based on Mindlin-Engesser formulation. Department of Civil Engineering, University of Queensland, 1993.

Y, Xiang, ed. Plate vibration with arbitrarily oriented stiffners based on Mindlin-Engesser formulation. University of Queensland, Dept. of Civil Engineering, 1993.

Goodarz, Ahmadi, Kehoe Mike, and United States. National Aeronautics and Space Administration., eds. Passive vibration control of airborne equipment using a circular steel ring. National Aeronautics and Space Administration, 1997.

L, Krantz T., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structures and the application to the reduction of gearbox vibration. National Aeronautics and Space Administration, 1995.

L, Krantz T., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structures and the application to the reduction of gearbox vibration. National Aeronautics and Space Administration, 1995.

Craig, L. D. Deflections of a uniformly loaded circular plate with multiple support points. National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

Collins, J. Scott. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. Langley Research Center, 1990.

R, Johnson Eric, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Dept., and Langley Research Center, eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

R, Johnson Eric, Virginia Polytechnic Institute and State University. Engineering Science and Mechanics Dept., and Langley Research Center, eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

R, Johnson Eric, NASA-Virginia Tech Composites Program, Virginia Polytechnic Institute and State University. Center for Composite Materials and Structures., and Langley Research Center. Landing and Impact Dynamics Branch., eds. Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. College of Engineering, Virginia Polytechnic Institute and State University, 1989.

Flaga, Andrzej. Wind vortex-induced excitation and vibration of slender structures: Single structure of circular cross-section normal to flow. Cracow University of Technology, 1996.

M, Morales Adolfo, and Dryden Flight Research Facility, eds. The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.

H, Williams James, Lee Samson S, and Lewis Research Center, eds. Stress waves in an isotropic elastic plate excited by a circular transducer. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Facility, Dryden Flight Research, ed. Stress concentration around a small circular hole in the HiMAT composite plate. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

R, Emeric P., and Institute for Computer Applications in Science and Engineering., eds. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Puttonen, Jari. Boundary element analysis for dynamic loading of a circular plate on an elastic medium. Teknillisten tieteiden akatemia, 1987.

Thomas, Banks H., and Institute for Computer Applications in Science and Engineering., eds. The estimation of material and patch parameters in a PDE-based circular plate model. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Anderson, Melvin S. Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate asemblies. Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., ed. Deflection of a circular liquid jet on a flat plate perpendicular to the flow direction. National Aeronautics and Space Administration, 1988.

Yuan, Weixing. Buckling and vibration of compact laminated and sandwich plate structures by a refined spline finite strip analysis. University of Birmingham, 1999.

Center, Langley Research, ed. Mobility power flow analysis of coupled plate structure subjected to mechanical and acoustic excitation. National Aeronautics and Space Administration, Langley Research Center, 1992.

Mohd, Sabarudin bin. Vibration and buckling analysis of laminated plate and shell structures by thin and shear deformable curved finite strips. University of Birmingham, 1990.

Noël, Jean-Marc A. Modes of vibration in an ideal fluid between infinite soft and rigid concentric and eccentric circular cylindrical boundaries. Laurentian University, 1994.

1949-, Devlin Frank J., and Cheeseman James R. 1963-, eds. VCD spectroscopy for organic chemists. CRC Press, 2012.

Yu, Shudong. Free vibration and buckling of laminated rectangular plates and isotropic open circular cylindrical shells. 1995.

Dorie, Carmine. Whole Body Vibration No Need Vibration Plate for Good Health: Human Body Vibration Book. Independently Published, 2020.

Mustafa, B. A. J. Free vibration analysis of stiffened circular shells. 1986.

Chen, Shoei-Sheng. Flow-Induced Vibration of Circular Cylindrical Structures. Springer, 1996.

Flow-induced vibration of circular cylindrical structures. Hemisphere Pub. Corp., 1987.

National Aeronautics and Space Administration (NASA) Staff. Minimization of the Vibration Energy of Thin-Plate Structures and the Application to the Reduction of Gearbox Vibration. Independently Published, 2018.

Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Interaction of acoustic waves generated by coupled plate. Center for Acoustics and Vibration, Florida Atlantic University, 1990.

National Aeronautics and Space Administration (NASA) Staff. Static and Vibration Analyses of General Wing Structures Using Equivalent Plate Models. Independently Published, 2018.

Wu, Zhonghui. Optimized Multi-Modes Mimo Positive Position Feedback Active Vibration for Plate Structure. GRIN Verlag GmbH, 2016.

National Aeronautics and Space Administration (NASA) Staff. Deflections of a Uniformly Loaded Circular Plate with Multiple Support Points. 1; Introduction. Independently Published, 2018.

National Aeronautics and Space Administration (NASA) Staff. Estimation of Material and Patch Parameters in a Pde-Based Circular Plate Model. Independently Published, 2018.