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1

W, Goodnight Thomas, Farkas Michael A, and NASA Glenn Research Center, eds. CM-2 environmental/modal testing of Spacehab racks. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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2

McNelis, Mark E. CM-2 environmental/modal testing of Spacehab racks. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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3

Boer, A. de. A study on methods to compare measured and calculated modal data. National Aerospace Laboratory, 1993.

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4

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

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5

M, Adelman Howard, Haftka Raphael T, Virginia Polytechnic Institute and State University, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Sensitivity Analysis in Engineering: Proceedings of a symposium. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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6

Schenk, Axel. Modal identification of a deployable space truss. National Aeronautics and Space Administration, Langley Research Center, 1990.

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7

S, Pappa Richard, and Langley Research Center, eds. Modal identification of a deployable space truss. National Aeronautics and Space Administration, Langley Research Center, 1990.

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8

Pressure Vessels and Piping Conference (1989 Honolulu, Hawaii). Application of modal analysis techniques to seismic and dynamic loadings: Presented at the 1989 ASME Pressure Vessels and Piping Conference--JSME co-sponsorship, Honolulu, Hawaii, July 23-27, 1989. American Society of Mechanical Engineers, 1989.

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9

Forbes, P. D. A dynamic matrix reduction process which facilitates modal frequency response analysis with the MARC system. National Engineering Laboratory, 1991.

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10

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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11

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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12

G, Gilbert Michael, and Langley Research Center, eds. STS-74/Mir Photogrammetric Appendage Structural Dynamics Experiment preliminary data analysis. National Aeronautics and Space Administration, Langley Research Center, 1997.

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13

L, Mattern Duane, Le Dzu K, and United States. National Aeronautics and Space Administration., eds. Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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14

L, Mattern Duane, Le Dzu K, and United States. National Aeronautics and Space Administration., eds. Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine. National Aeronautics and Space Administration, 1996.

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15

Faliva, Mario, and Maria Grazia Zoia, eds. Dynamic Model Analysis. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-85996-3.

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16

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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17

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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18

Deoss, Dister Leroy. A simulation model for dynamic system availability analysis. Available from the National Technical Information Service, 1989.

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19

Paxson, D. E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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20

United States. National Aeronautics and Space Administration., ed. Numerical model of solar dynamic radiator for parametric analysis. National Aeronautics and Space Administration, 1989.

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21

United States. National Aeronautics and Space Administration., ed. Numerical model of solar dynamic radiator for parametric analysis. National Aeronautics and Space Administration, 1989.

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22

Rick, Lind, Brenner Martin J, and United States. National Aeronautics and Space Administration., eds. Correlation filtering of modal dynamics using the Laplace wavelet. National Aeronautics and Space Administration, 1997.

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23

Rick, Lind, Brenner Martin J, and United States. National Aeronautics and Space Administration., eds. Correlation filtering of modal dynamics using the Laplace wavelet. National Aeronautics and Space Administration, 1997.

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24

Nalecz, Andrzej G. Sensitivity analysis of vehicle tripped rollover model. U.S. Dept. of Transportation, National Highway Traffic Safety Administration, 1988.

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25

Michelsen, Finn Are. A dynamic mechanistic model and model-based analysis of a continuous Kamyr digester. Universitetet i Trondheim, 1995.

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26

L, Wicks Alfred, Society for Experimental Mechanics (U.S.), and International Modal Analysis Conference (19th : 2001 : Kissimmee, Fla.), eds. Proceedings of IMAC-XIX : a conference on structural dynamics: February 5-8, 2001, Hyatt Orlando, Kissimmee, Florida. Society for Experimental Mechanics, 2001.

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27

Chen, J. Robust model-based fault diagnosis for dynamic systems. Kluwer Academic Publishers, 1999.

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28

Koh, Hyun M. A mixed Eulerian-Lagrangian model for the analysis of dynamic fracture. University of Illinois at Urbana-Champaign, 1986.

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29

International, Modal Analysis Conference (18th 2000 San Antonio Texas). IMAC XVIII: Proceedings of IMAC-XVIII: a conference on structural dynamics : February 7-10, 2000, the Westin La Cantera Resort, San Antonio, Texas. Society for Experimental Mechanics, 2000.

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30

Brock, William A. A dynamic structural model for stock return volatility and trading volume. National Bureau of Economic Research, 1995.

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31

Dippner, J. W. A Lagrangian model of phytoplankton growth dynamics: A sensitivity analysis. Commission of the European Communities, 1991.

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32

International Seminar on Modal Analysis (15th 1990 Katholieke Universiteit te Leuven). Proceedings of the 15th International Seminar on Modal Analysis: 19-21 September 1990. Katholieke Universiteit Leuven, Faculty of Applied Sciences, Dept. of Mechanical Engineering, Mechanical Construction and Production Division., 1990.

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33

International Seminar on Modal Analysis (13th 1988 Katholieke Universiteit te Leuven). Proceedings of the 13th International Seminar on Modal Analysis: 19-23 September 1988. Edited by Sas Paul and Katholieke Universiteit te Leuven (1970- ). Afdeling Mechanische Konstruktie en Produktie. Katholieke Universiteit Leuven, Fakulteit der Toegepaste Wetenschappen, Departement Werktuigkunde, Afdeling Mechanische Konstruktie en Produktie, 1988.

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34

Grazia, Zoia Maria, and Faliva Mario, eds. Dynamic model analysis: Advanced matrix methods and unit-root econometrics representation theorems. 2nd ed. Springer, 2009.

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35

Kabundi, Alain N. France in the global economy: A structural approximate dynamic factor model analysis. International Monetary Fund, European Dept., 2007.

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36

Mickelson, William T. Aggregate dynamic analysis model (ADAM) for Air Force Enlisted personnel: Technical documentation. Rand, 1989.

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37

United States. National Aeronautics and Space Administration., ed. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. National Aeronautics and Space Administration, 1993.

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38

Mickelson, William T. Aggregate dynamic analysis model (ADAM) for Air Force Enlisted personnel: User's guide. Rand, 1989.

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39

United States. National Aeronautics and Space Administration., ed. An extended supersonic combustion model for the dynamic analysis of hypersonic vehicles. National Aeronautics and Space Administration, 1993.

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40

V, Kaza K. R., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Analysis of an unswept propfan blade with a semiempirical dynamic stall model. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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41

Nalecz, Andrzej G. Development and analysis of intermediate tripped vehicle rollover model (ITRS). U.S. Dept. of Transportation, National Highway Traffic Safety Administration, 1989.

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42

Gronet, M. J. Preliminary design, analysis, and costing of a dynamic model of the NASA space station. Langley Research Center, 1987.

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43

Center, Langley Research, ed. Modeling the benchmark active control technology wind-tunnel model for active control design applications. National Aeronautics and Space Administration, Langley Research Center, 1998.

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44

Mocan, H. Naci. Business cycles and fertility dynamics in the U.S.: A vector-autoregressive model. National Bureau of Economic Research, 1989.

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45

CM-2 environmental/modal testing of Spacehab racks. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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46

CM-2 environmental/modal testing of Spacehab racks. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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47

Advanced Gun System (AGS) Dynamic Characterization: Modal Test and Analysis, High-Frequency Analysis. Storming Media, 1999.

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48

Frequency based localization of structural discrepancies. Charles Stark Draper Laboratory, 1988.

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49

Nuyts, Jan. Analyses of the Modal Meanings. Edited by Jan Nuyts and Johan Van Der Auwera. Oxford University Press, 2014. http://dx.doi.org/10.1093/oxfordhb/9780199591435.013.1.

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Abstract:
This article deals with the semantic analysis of the notion of modality, surveying the most important traditional views in linguistics. After pointing out the problems encountered in the literature in trying to define the category, it first discusses the in the literature most common basic types of modality, namely, dynamic modality, deontic modality, and epistemic modality, as well as the less common basic category of boulomaic modality. It then goes on to survey a variety of alternative views on how the semantic domain of modality may be organized. The article also considers the types of cri
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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 ... National Aeronautics and Space Administration, 1997.

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