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1

Distinguished Instructor Short Course (2nd 1999 Tulsa, Okla.). The seismic velocity model as an interpretation asset. Tulsa, OK: Society of Exploration Geophysicists, 1998.

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2

Simon, Frederick F. Jet model for slot film cooling with effect of free-stream and coolant turbulence. Cleveland, Ohio: Lewis Research Center, 1986.

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3

Berry, John D. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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4

Laenen, Antonius. Simulation of three lahars in the Mount St. Helens area, Washington using a one-dimensional, unsteady-state streamflow model. Portland, Or: Dept. of the Interior, U.S. Geological Survey, 1988.

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5

Swift, Calvin T. Development of a validation model for the Defense meteorological satellite program's special sensor microwave imager. [Washington, DC: National Aeronautics and Space Administration, 1990.

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6

Khazanehdari, Jalal. A model of the velocity structure of the Ivrea-Verbano lower crustal section, Northern Italy. Manchester: University of Manchester, 1996.

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7

Bollinger, G. A. Development of a velocity model for locating aftershocks in the Sierra Pie de Palo region of western Argentina. Washington: U.S. G.P.O., 1988.

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8

Lemon, Michael R. Comparison of Los Alamos National Laboratory (LANL) Parallel Ocean Program (POP) model velocity fields with Pacific surface drifter measurements. Monterey, Calif: Naval Postgraduate School, 1997.

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9

Fernando, Alvarez. On the sluggish response of prices to money in an inventory-theoretic model of money demand. Cambridge, Mass: National Bureau of Economic Research, 2003.

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10

Pelton, Jimmy W. A comparison of output from the Los Alamos National Laboratory (LANL) Parallel Ocean Program (POP) model with surface velocity data from drifting Buoys in the North Atlantic Ocean. Monterey, Calif: Naval Postgraduate School, 2000.

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11

Schwanke, Peter. Implementation into DIVIMP of a drift-kinetic model derived from the Fokker-Planck equation to examine the parallel-to-B velocity component of impurity ions in divertor-tokamak plasmas. Toronto: Department of Aerospace Science and Engineering, University of Toronto, 2001.

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12

Barna, P. S. Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel: Progress report on the D.S.M.A. design. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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13

Jones, Ian. An Introduction to: Velocity Model Building. EAGE Publications bv, 2010. http://dx.doi.org/10.3997/9789073781849.

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14

Shuttle data book, SRM fragment velocity model. [Washington, DC: National Aeronautics and Space Administration, 1989.

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15

Robinson, Enders A. Seismic Velocity Analysis and the Convolutional Model. Pearson Education, Limited, 1988.

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16

1956-, Jones Ian Frederick, ed. Prestack depth migration and velocity model building. Tulsa, Okla., U.S.A: Society of Exploration Geophysicists, 2008.

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17

Jones, Ian. ebook - An Introduction to: Velocity Model Building. EAGE Publications bv, 2014. http://dx.doi.org/10.3997/9789073834958.

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18

P, Goel, Chai J. C, and United States. National Aeronautics and Space Administration, eds. A transport model of the turbulent scalar-velocity: Status report. Milwaukee, Wis: Dept. of Mechanical Engineering, University fo Wisconsin--Milwaukee, 1987.

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19

HIVEL2D, a two-dimensional flow model for high-velocity channels. Vicksburg, MS: US Army Corps of Engineers, Waterways Experiment Station, 1994.

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20

C, Berger Rutherford, and U.S. Army Engineer Waterways Experiment Station., eds. HIVEL2D, a two-dimensional flow model for high-velocity channels. Vicksburg, MS: US Army Corps of Engineers, Waterways Experiment Station, 1994.

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21

P, Goel, Chai John C, and United States. National Aeronautics and Space Administration., eds. A transport model of the turbulent scalar-velocity: Status report. Milwaukee, Wis: Dept. of Mechanical Engineering, University fo Wisconsin--Milwaukee, 1987.

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22

HIVEL2D, a two-dimensional flow model for high-velocity channels. Vicksburg, MS: US Army Corps of Engineers, Waterways Experiment Station, 1994.

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23

B, Gatski T., Speziale C. G. 1948-, and Langley Research Center, eds. Towards a rational model for the triple velocity correlations of turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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24

B, Gatski T., Speziale C. G. 1948-, and Langley Research Center, eds. Towards a rational model for the triple velocity correlations of turbulence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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25

U.S. Army Engineer Waterways Experiment Station., ed. Guadalupe River and bypass culvert, San Jose, California: Hydraulic model investigation. Vicksburg, Miss: US Army Corps of Engineers, Waterways Experiment Station, 1998.

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26

U.S. Army Engineer Waterways Experiment Station., ed. Guadalupe River and bypass culvert, San Jose, California: Hydraulic model investigation. Vicksburg, Miss: US Army Corps of Engineers, Waterways Experiment Station, 1998.

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27

Antonio, Villaseñor, Benz Harley M, and Geological Survey (U.S.), eds. Subduction zone and crustal dynamics of western Washington: A tectonic model for earthquake hazards evaluation. [Reston, Va.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1999.

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28

Antonio, Villaseñor, Benz Harley M, and Geological Survey (U.S.), eds. Subduction zone and crustal dynamics of western Washington: A tectonic model for earthquake hazards evaluation. [Reston, Va.?]: U.S. Dept. of the Interior, U.S. Geological Survey, 1999.

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29

A, Jackson K., and United States. National Aeronautics and Space Administration., eds. Orientation and velocity dependence of the nonequilibrium partition coefficient. [Washington, DC: National Aeronautics and Space Administration, 1995.

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30

Center, Langley Research, and U.S. Army Aviation and Troop Command., eds. Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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31

Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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32

G, Seasholtz Richard, and United States. National Aeronautics and Space Administration., eds. Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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33

G, Seasholtz Richard, and United States. National Aeronautics and Space Administration., eds. Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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34

Shultz, Phil. The Seismic Velocity Model as an Interpretation Asset (Distinguished Instructor Series, Number 2). Society Of Exploration Geophysicists, 1999.

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35

G, Seasholtz Richard, and United States. National Aeronautics and Space Administration., eds. Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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36

Velocity and pressure characteristics of a model SSME high pressure fuel turbopump: Final report. [Washington, DC: National Aeronautics and Space Administration, 1991.

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37

Gnewuch, Scot C. Investigation of velocity and anelastic attenuation structures of the shallow crust in New England by time domain modeling of Rg waves. 1987.

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38

W, Elliott Joe, United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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39

C.J.A.P. Martins. Defect Evolution in Cosmology and Condensed Matter: Quantitative Analysis with the Velocity-Dependent One-Scale Model. Springer, 2016.

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40

United States. National Aeronautics and Space Administration., ed. LDV measurements in an annular combustor model. West Lafayette, Ind: Purdue University, School of Aeronautics and Astronautics, 1989.

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41

United States. National Aeronautics and Space Administration., ed. LDV measurements in an annular combustor model. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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42

Turbulence measurements on a flap-edge model: Final report : NASA-Ames university consortium, NCC2-5140. [Washington, DC: National Aeronautics and Space Administration, 1996.

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43

Effects of yaw and pitch motion on model attitude measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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44

S, Tripp John, Finley Tom D, and Langley Research Center, eds. Effects of yaw and pitch motion on model attitude measurements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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45

Thomas, Nehrkorn, Grassotti Christopher, and United States. National Aeronautics and Space Administration., eds. Distortion representation of forecast errors for model skill assessment and objective analysis: Technical report. [Washington, DC: National Aeronautics and Space Administration, 1996.

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46

United States. National Aeronautics and Space Administration., ed. Atmospheric probe model: Construction and wind tunnel tests : final report : grant no. NCC 2-935. [Washington, DC: National Aeronautics and Space Administration, 1998.

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47

Atmospheric probe model: Construction and wind tunnel tests : final report : grant no. NCC 2-935. [Washington, DC: National Aeronautics and Space Administration, 1998.

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48

J, Kessler Donald, and United States. National Aeronautics and Space Administration., eds. A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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49

A Comparison Of Output From The Los Alamos National Laboratory (LANL) parallel Ocean Program (POP) Model With Surface Velocity Data From Drifting Buoys in the North Atlantic Ocean. Storming Media, 2000.

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50

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, ed. Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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