Books on the topic 'Free vibration of plate'

Wu, K. Chauncey. Free vibration of hexagonal panels simply supported at discrete points. National Aeronautics and Space Administration, Langley Research Center, 1991.

Ayowole, Oyediran Abraham, and George C. Marshall Space Flight Center., eds. Free vibration of rectangular plates with a small initial curvature: Final report. Marshall Space Flight Center, 1988.

A, Kolkailah Faysal, Elghandour Eltahry I, and United States. National Aeronautics and Space Administration., eds. Modal analysis of embedded passive damping materials in composite plates with different orientations: Final report for NASA-Dryden Flight Research Center, joint research interchange, May 1, 1997-July 24, 1998. National Aeronautics and Space Administration, 1998.

A, Kolkailah Faysal, Elghandour Eltahry I, and United States. National Aeronautics and Space Administration., eds. Modal analysis of embedded passive damping materials in composite plates with different orientations: Final report for NASA-Dryden Flight Research Center, joint research interchange, May 1, 1997-July 24, 1998. National Aeronautics and Space Administration, 1998.

Abbassian, F. Free vibration benchmarks. NAFEMS, 1987.

Hagedorn, Peter. Vibrations and Impedances of Rectangular Plates with Free Boundaries. Springer Berlin Heidelberg, 1986.

Hagedorn, Peter, Klaus Kelkel, and Jörg Wallaschek. Vibrations and Impedances of Rectangular Plates with Free Boundaries. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82906-2.

Klaus, Kelkel, and Wallaschek J. 1960-, eds. Vibrations and impedances of rectangular plates with free boundaries. Springer-Verlag, 1986.

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.

United States. National Aeronautics and Space Administration., ed. Correlation of finite element free vibration predictions using random vibration test data. National Aeronautics and Space Administration, 1994.

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.

Karunendiran, Seevaratnam. Free vibration analysis of rotor-bearing systems. National Library of Canada, 1996.

Center, Lewis Research, ed. Free vibrations of delaminated beams. National Aeronautics and Space Administration, Lewis Research Center, 1992.

N, Virgin L., Rizzi Stephen A, and Langley Research Center, eds. Free vibration of thermally loaded panels including initial imperfections and post-buckling effects. National Aeronautics and Space Administration, Langley Research Center, 1994.

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.

Lai, Liping. Study of free vibration of aluminium honeycomb panels. National Library of Canada, 2002.

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.

D, Carden Huey, Peters Jeanne M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Free vibrations of thin-walled semicircular graphite-epoxy composites. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

D, Carden Huey, Peters Jeanne M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Free vibrations of thin-walled semicircular graphite-epoxy composites. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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.

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.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. The design, qualification and maintenance of vibration-free landing gear. AGARD, 1996.

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.

United States. National Aeronautics and Space Administration, ed. Free vibration and dynamic response analysis of spinning structures: Final report. National Aeronautics and Space Administration, 1986.

Duxbury, Geoffrey. Infrared vibration-rotation spectroscopy: From free radicals to the infrared sky. John Wiley, 1999.

Gotsis, Pascal K. Free vibration of fiber composite thin shells in a hot environment. National Aeronautics and Space Administration, 1995.

S, Najjar Bassam, and United States. National Aeronautics and Space Administration., eds. Passive damping concepts for free and forced member and grillage vibration. Old Dominion University Research Foundation, 1988.

Kogan, M. N. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate). National Aeronautics and Space Administration, Langley Research Center, 1997.

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.

Noor, Ahmed Khairy. Free vibrations of thin-walled semicircular graphite-epoxy composite frames. Langley Research Center, 1990.

Gotsis, Pascal K. Laminated thin shell structures subjected to free vibration in a hygrothermal environment. National Aeronautics and Space Administration, 1994.

Gotsis, Pascal K. Laminated thin shell structures subjected to free vibration in a hygrothermal environment. National Aeronautics and Space Administration, 1994.

K, Muyundo David, Old Dominion University. Research Foundation., and Langley Research Center, eds. Passive damping concepts for tubular beams with partial rotational and translational end restraints. Old Dominion University Research Foundation, 1991.

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

N, Kogan M., and Langley Research Center, eds. Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): Final report. National Aeronautics and Space Administration, Langley Research Center, 1999.

Noor, Ahmed Khairy. Mixed finite element models for free vibrations of thin-walled beams. Langley Research Center, 1989.

Carney, Kelly S. Free-vibration characteristics and correlation of a space station split-blanket solar array. National Aeronautics and Space Administration, 1989.