Книги з теми "Vibration load"

Chouw, Nawawi, and Günther Schmid. Wave propagation Moving load – Vibration Reduction. London: CRC Press, 2021. http://dx.doi.org/10.1201/9781003211372.

International Workshop Wave 2000 (13-15 December 2000 Bochum, Germany). Wave 2000: Wave propagation, moving load, vibration reduction. Rotterdam, Netherlands: A.A. Balkema, 2000.

Fleming, David P. Transient vibration prediction for rotors on ball bearings using load-dependent non-linear bearing stiffness. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Alliance, National Steel Bridge. V-load analysis: An approximate procedure, simplified and extended, for determining moments and shears in designing horizontally-curved open-framed highway bridges. Chicago, Ill: National Steel Bridge Alliance, 1996.

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

International, Workshop Wave 2002 (2002 Okayamaken Japan). Wave propagation, moving load, vibration reduction: Proceedings of the International Workshop WAVE 2002, Okayama, Japan, 18-20 September 2002. Lisse: Balkema, 2003.

Issa, Mohsen A. Construction loads and vibrations. [Edwardsville, IL]: Illinois Transportation Research Center, Illinois Dept. of Transportation, 1998.

Vibration of solids and structures under moving loads. 3rd ed. London: Thomas Telford, 1999.

Balendra, T. Vibration of Buildings to Wind and Earthquake Loads. London: Springer London, 1993.

Balendra, T. Vibration of Buildings to Wind and Earthquake Loads. London: Springer London, 1993. http://dx.doi.org/10.1007/978-1-4471-2055-1.

Vibration of buildings to wind and earthquake loads. London: Springer-Verlag, 1993.

Bajer, Czesław I. Numerical Analysis of Vibrations of Structures under Moving Inertial Load. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

Bajer, Czesław I., and Bartłomiej Dyniewicz. Numerical Analysis of Vibrations of Structures under Moving Inertial Load. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-29548-5.

Willford, M. R. A design guide for footfall induced vibration of structures: [a tool for designers to engineer the footfall vibration characteristics of buildings or bridges]. Camberley: Concrete Society for The Concrete Centre, 2006.

Squire, Vernon A. Moving Loads on Ice Plates. Dordrecht: Springer Netherlands, 1996.

Bornsteiln, A. Vibration and buckling tests of stringer-stiffened cylindrical shells subjected to non-uniform axial loading. Haifa, Israel: Technion - Israel Institute of Technology, 1991.

Szmidla, Janusz. Drgania swobodne i stateczność układów smukłych poddanych obciążeniu swoistemu. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2000.

Szmidla, Janusz. Drgania swobodne i stateczność układów smukłych poddanych obciążeniu swoistemu. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2000.

Shukla, A. Dynamic failure of materials and structures / Arun Shukla, Guruswami Ravichandran, Yapa D.S. Rajapakse, editors,. New York: Springer, 2010.

Kulisiewicz, Maciej. Modeling and identification of nonlinear mechanical systems under dynamic complex loads. Wrocław: Oficyna Wydawnicza Politechniki Wrocławskiej, 2005.

Yates, John E. Analysis of the surface load and radiated sound of a vibrating airfoil with application to the experiment of Brooks. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Stephens, Jerry E. Performance of steel pipe pile-to-concrete bent cap connections subject to seismic or high transverse loading, phase II: Project summary report. Helena, Mont: Montana Dept. of Transportation, 2005.

Stephens, Jerry E. Performance of steel pipe pile-to-concrete bent cap connections subject to seismic or high transverse loading, phase II: Final report. Helena]: Montana Dept. of Transportation, 2005.

Stredulinsky, David C. The prediction of strength and natural frequencies of vibration of a model submarine propeller subjected to large centrifugal loads in a wind tunnel. Dartmouth, N.S: Defence Research Establishment Atlantic, 1992.

ASME Pressure Vessels and Piping Conference. (1988 Pittsburgh, Pa.). Application of modal analysis to extreme loads: Presented at 1988 ASME Pressure Vessels and Piping Conference, Pittsburgh, Pennsylvania, June 19-23, 1988 : sponsored by the Pressure Vessels and Piping Division, ASME. New York: American Society of Mechanical Engineers, 1988.

Johnson, Peter W., and Martin G. Cherniack. Vibration. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780190662677.003.0013.

J, Zakrajsek James, and NASA Glenn Research Center, eds. Minimizing load effects on NA4 gear vibration diagnostic parameter. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

P, Townsend Dennis, Oswald Fred B, and United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.

P, Townsend Dennis, Oswald Fred B, and United States. National Aeronautics and Space Administration., eds. Experimental and analytical evaluation of dynamic load and vibration of a 2240-kW (3000-hp) rotorcraft transmission. [Washington, DC: National Aeronautics and Space Administration, 1987.

Paeglīte, Ilze. Kustīgās slodzes dinamiskās iedarbes uz autoceļu tiltiem eksperimentāla izpēte un novērtējums. RTU Press, 2021. http://dx.doi.org/10.7250/9789934227028.

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. Blacksburg, Va: 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. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 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. Washington, D.C: 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. Blacksburg, Va: 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. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1989.

Ravi, Margasahayam, and John F. Kennedy Space Center., eds. Validation of a deterministic vibroacoustic response prediction model. Kennedy Space Center, Fla: National Aeronautics and Space Administration, John F. Kennedy Space Center, 1997.

Ravi, Margasahayam, and John F. Kennedy Space Center., eds. Validation of a deterministic vibroacoustic response prediction model. Kennedy Space Center, Fla: National Aeronautics and Space Administration, John F. Kennedy Space Center, 1997.

V, Sankewitsch, and Langley Research Center, eds. Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Vibroacoustic response of pad structures to space shuttle launch acoustic loads. [Washington, DC: National Aeronautics and Space Administration, 1995.

E, Caimi Raoul, and United States. National Aeronautics and Space Administration., eds. Vibroacoustic response of pad structures to space shuttle launch acoustic loads. [Washington, DC: National Aeronautics and Space Administration, 1995.

C, Jenkins Robert, and United States. National Aeronautics and Space Administration., eds. Experimental analysis of thread movement in bolted connections due to vibrations: Research project NAS8-39131 : final report, August 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

C, Jenkins Robert, and United States. National Aeronautics and Space Administration., eds. Experimental analysis of thread movement in bolted connections due to vibrations: Research project NAS8-39131 : final report. [Washington, DC]: National Aeronautics and Space Administration, 1994.

C, Jenkins Robert, and United States. National Aeronautics and Space Administration., eds. Experimental analysis of thread movement in bolted connections due to vibrations: Final report. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Numerical Analysis Of Vibrations Of Structures Under Moving Inertial Load. Springer, 2012.

Bajer, Czesław I. I., and Bartłomiej Dyniewicz. Numerical Analysis of Vibrations of Structures under Moving Inertial Load. Springer, 2016.

L, Wilbur Matthew, U.S. Army Research Laboratory., and Langley Research Center, eds. Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

R, Pamidi P., and Lewis Research Center, eds. NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems: Final report. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

United States. National Aeronautics and Space Administration., ed. System identification of damped truss-like space structures. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Facility, Dryden Flight Research, ed. Higher harmonic control analysis for vibration reduction of helicopter rotor systems. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1994.