Книги з теми "Finite element modal updating"
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Friswell, M. I., and J. E. Mottershead. Finite Element Model Updating in Structural Dynamics. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-015-8508-8.
Повний текст джерелаE, Mottershead J., ed. Finite Element Model Updating in Structural Dynamics. Dordrecht: Springer Netherlands, 1995.
Знайти повний текст джерелаFriswell, M. I. Finite element model updating in structural dynamics. Dordrecht: Kluwer Academic Publishers, 1995.
Знайти повний текст джерелаMarwala, Tshilidzi. Finite-element-model Updating Using Computional Intelligence Techniques. London: Springer London, 2010. http://dx.doi.org/10.1007/978-1-84996-323-7.
Повний текст джерелаMarwala, Tshilidzi, Ilyes Boulkaibet, and Sondipon Adhikari. Probabilistic Finite Element Model Updating Using Bayesian Statistics. Chichester, UK: John Wiley & Sons, Ltd, 2016. http://dx.doi.org/10.1002/9781119153023.
Повний текст джерелаPampalone, Michael R. Development, correlation and updating of a finite element model of the OH-6A helicopter. Monterey, Calif: Naval Postgraduate School, 1996.
Знайти повний текст джерелаCraig, Roy R. Substructure system identification for finite element model updating: Final report, NASA grant no. NAG8-1130. Austin, Tex: Center for Aeronautical Research, Bureau of Engineering Research, the University of Texas at Austin, 1997.
Знайти повний текст джерелаFriswell, Michael Ian. Updating finite element models using measured vibration data. Birmingham: Aston University. Department of Mechanical and Production Engineering, 1990.
Знайти повний текст джерелаRoss, C. T. F. Finite element techniques in structural mechanics. Chichester, England: Albion Pub., 1996.
Знайти повний текст джерелаC, Steele N., ed. Finite element techniques in structural mechanics. Chichester: Albion Publishing, 1996.
Знайти повний текст джерелаBaumeister, Kenneth J. Modal element method for potential flow in nonuniform ducts: Combining closed form analysis with CFD. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаDunn, Shane A. Issues concerning the updating of the finite-element models from experimental data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаDunn, Shane A. Issues concerning the updating of the finite-element models from experimental data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Знайти повний текст джерелаE, McGowan P., and Langley Research Center, eds. Locating damaged members in a truss structure using modal data: A demonstration experiment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Знайти повний текст джерелаJ, Baumeister Kenneth, and United States. National Aeronautics and Space Administration., eds. Acoustic scattering from ellipses by the modal element method. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаKnott, George Anthony. A modal analysis of the violin using MSC/NASTRAN and PATRAN. Monterey, Calif: Naval Postgraduate School, 1987.
Знайти повний текст джерелаMV2, International Conference. New advances in modal synthesis of large structures: Non-linear damped and non-deterministic cases : proceedings of the International Conference MV2, Lyon France, 5-6 October 1995. Rotterdam: A.A. Balkema, 1997.
Знайти повний текст джерелаS, Pappa Richard, and Langley Research Center, eds. Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Знайти повний текст джерелаS, Pappa Richard, and Langley Research Center, eds. Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Знайти повний текст джерелаS, Pappa Richard, and Langley Research Center, eds. Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Correlation of finite element free vibration predictions using random vibration test data. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаH, Mirick Paul, Langston Chester W, and Langley Research Center, eds. Rotating shake test and modal analysis of a model helicopter rotor blade. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаShutty, Michael Allen. Dynamic modeling and modal analysis of an air-to-air missile. Monterey, California: Naval Postgraduate School, 1991.
Знайти повний текст джерелаHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.
Знайти повний текст джерелаHamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаM, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаBaumeister, Kenneth J. Modal ring method for the scattering of sound. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1993.
Знайти повний текст джерелаM, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаL, Kreider Kevin, Lewis Research Center, and American Society of Mechanical Engineers. Winter Meeting., eds. Modal ring method for the scattering of sound. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Nondestructive analysis and development: Final report. Orlando, Fla: Dept. of Mechanical and Aerospace Engineering, University of Central Florida, 1993.
Знайти повний текст джерелаFinite Element Model Updating Using Antiresonant Frequencies. Storming Media, 2000.
Знайти повний текст джерелаMarwala, Tshilidzi. Finite Element Model Updating Using Computational Intelligence Techniques: Applications to Structural Dynamics. Springer, 2014.
Знайти повний текст джерелаMarwala, Tshilidzi. Finite Element Model Updating Using Computational Intelligence Techniques: Applications to Structural Dynamics. Springer, 2010.
Знайти повний текст джерелаFinite Element Model Updating and Damage Detection Using Artificial Boundary Conditions. Storming Media, 1999.
Знайти повний текст джерелаMarwala, Tshilidzi, Sondipon Adhikari, and Ilyes Boulkaibet. Probabilistic Finite Element Model Updating Using Bayesian Statistics: Applications to Aeronautical and Mechanical Engineering. Wiley & Sons, Limited, John, 2016.
Знайти повний текст джерелаMarwala, Tshilidzi, Sondipon Adhikari, and Ilyes Boulkaibet. Probabilistic Finite Element Model Updating Using Bayesian Statistics: Applications to Aeronautical and Mechanical Engineering. Wiley & Sons, Limited, John, 2016.
Знайти повний текст джерелаMarwala, Tshilidzi, Sondipon Adhikari, and Ilyes Boulkaibet. Probabilistic Finite Element Model Updating Using Bayesian Statistics: Applications to Aeronautical and Mechanical Engineering. Wiley & Sons, Incorporated, John, 2016.
Знайти повний текст джерелаMarwala, Tshilidzi, Sondipon Adhikari, and Ilyes Boulkaibet. Probabilistic Finite Element Model Updating Using Bayesian Statistics: Applications to Aeronautical and Mechanical Engineering. Wiley & Sons, Incorporated, John, 2016.
Знайти повний текст джерелаDevelopment, Correlation and Updating of a Finite Element Model of the OH-6A Helicopter. Storming Media, 1996.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Issues Concerning the Updating of Finite-Element Models from Experimental Data. Independently Published, 2018.
Знайти повний текст джерелаKaouk, Mohamed. Structural damage assessment and finite element model refinement using measured modal data. 1993.
Знайти повний текст джерелаPrediction of Modal Characteristics of Orthotropic Curved Panel by Using Finite Element Method. Tiruchengode, India: ASDF International, 2017.
Знайти повний текст джерелаFiniteElementModel Updating Using Computational Intelligence Techniques. Springer, 2010.
Знайти повний текст джерелаCorrelation of finite element free vibration predictions using random vibration test data. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаModal analysis of UH-60A instrumented rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Знайти повний текст джерелаA Modal Approximation for the Mutual Radiation Impedance for Spherical Sources and Acoustic Wave Scattering Using an Improved Atila Finite Element Code. Storming Media, 1999.
Знайти повний текст джерелаNondestructive analysis and development: Final report. Orlando, Fla: Dept. of Mechanical and Aerospace Engineering, University of Central Florida, 1993.
Знайти повний текст джерелаIdentification of rotorcraft structural dynamics from flight and wind tunnel data: Final report covering the period February 1991 - August 1992, prepared under NASA-Ames agreement no. NAG 2-694 ... [Washington, DC: National Aeronautics and Space Administration, 1997.
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