Books on the topic 'Finite element modal updating'

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1

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.

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2

E, Mottershead J., ed. Finite Element Model Updating in Structural Dynamics. Dordrecht: Springer Netherlands, 1995.

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3

Friswell, M. I. Finite element model updating in structural dynamics. Dordrecht: Kluwer Academic Publishers, 1995.

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4

Marwala, Tshilidzi. Finite-element-model Updating Using Computional Intelligence Techniques. London: Springer London, 2010. http://dx.doi.org/10.1007/978-1-84996-323-7.

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5

Marwala, 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.

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6

Pampalone, Michael R. Development, correlation and updating of a finite element model of the OH-6A helicopter. Monterey, Calif: Naval Postgraduate School, 1996.

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7

Craig, 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.

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8

Friswell, Michael Ian. Updating finite element models using measured vibration data. Birmingham: Aston University. Department of Mechanical and Production Engineering, 1990.

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9

Ross, C. T. F. Finite element techniques in structural mechanics. Chichester, England: Albion Pub., 1996.

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10

C, Steele N., ed. Finite element techniques in structural mechanics. Chichester: Albion Publishing, 1996.

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11

Baumeister, 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.

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12

Dunn, 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.

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13

Dunn, 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.

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14

E, 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.

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15

J, 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.

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16

Knott, George Anthony. A modal analysis of the violin using MSC/NASTRAN and PATRAN. Monterey, Calif: Naval Postgraduate School, 1987.

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17

MV2, 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.

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18

S, 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.

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19

S, 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.

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20

S, 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.

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21

United 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.

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22

H, 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.

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23

Dynamic stiffness and substructures. London: Springer-Verlag, 1993.

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24

Shutty, Michael Allen. Dynamic modeling and modal analysis of an air-to-air missile. Monterey, California: Naval Postgraduate School, 1991.

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25

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Moffett Field, Calif: Ames Research Center, 1990.

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26

Hamade, 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.

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27

M, 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.

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28

Baumeister, Kenneth J. Modal ring method for the scattering of sound. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1993.

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29

M, 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.

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30

L, 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.

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31

United 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.

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32

Finite Element Model Updating Using Antiresonant Frequencies. Storming Media, 2000.

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33

Marwala, Tshilidzi. Finite Element Model Updating Using Computational Intelligence Techniques: Applications to Structural Dynamics. Springer, 2014.

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34

Marwala, Tshilidzi. Finite Element Model Updating Using Computational Intelligence Techniques: Applications to Structural Dynamics. Springer, 2010.

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35

Finite Element Model Updating and Damage Detection Using Artificial Boundary Conditions. Storming Media, 1999.

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36

Marwala, 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.

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37

Marwala, 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.

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38

Marwala, 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.

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39

Marwala, 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.

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40

Development, Correlation and Updating of a Finite Element Model of the OH-6A Helicopter. Storming Media, 1996.

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41

National Aeronautics and Space Administration (NASA) Staff. Issues Concerning the Updating of Finite-Element Models from Experimental Data. Independently Published, 2018.

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42

Kaouk, Mohamed. Structural damage assessment and finite element model refinement using measured modal data. 1993.

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43

Prediction of Modal Characteristics of Orthotropic Curved Panel by Using Finite Element Method. Tiruchengode, India: ASDF International, 2017.

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44

FiniteElementModel Updating Using Computational Intelligence Techniques. Springer, 2010.

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45

Jezequel. New Adv in Modal Synthesis Large. Taylor & Francis, 1997.

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46

Correlation of finite element free vibration predictions using random vibration test data. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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47

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.

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48

A Modal Approximation for the Mutual Radiation Impedance for Spherical Sources and Acoustic Wave Scattering Using an Improved Atila Finite Element Code. Storming Media, 1999.

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49

Nondestructive analysis and development: Final report. Orlando, Fla: Dept. of Mechanical and Aerospace Engineering, University of Central Florida, 1993.

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50

Identification 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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