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1

Meng-Sing, Liou, Hindman Richard G, and United States. National Aeronautics and Space Administration., eds. An approach for dynamic grids. National Aeronautics and Space Administration, 1994.

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2

AIAA Computational Fluid Dynamics Conference (11th 1993 Orlando, Fla.). 11th AIAA Computational Fluid Dynamics Conference: July 6-9, 1993, Orlando, Florida. AIAA, 1993.

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3

Kuhn, Gary D. Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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4

AIAA Computational Fluid Dynamics Conference (14th 1999 Norfolk, Virginia). A collection of technical papers: 14th AIAA Computational Fluid Dynamics Conference, Norfolk, Virginia, 28 June-1 July 1999. American Institute of Aeronautics and Astronautics, 1999.

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5

Agency, International Atomic Energy, ed. Integration of tracing with computational fluid dynamics for industrial process investigation: Final report of a co-ordinated research project 2001-2003. International Atomic Energy Agency, 2004.

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6

AIAA Computational Fluid Dynamics Conference (13th 1997 Snowmass Village, Co.). A collection of technical papers: 13th AIAA Computational Fluid Dynamics Conference ; Snowmass Village, CO, June 29-July 2, 1997. American Institute of Aeronautics and Astronautics, 1997.

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7

Wilcox, David C. Turbulence modeling for CFD. DCW Industries, Inc., 1993.

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8

Wilcox, David C. Turbulence modeling for CFD. 2nd ed. DCW Industries, 1998.

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9

Wilcox, David C. Turbulence modeling for CFD. DCW Industries, 1994.

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10

A, Ladd J., Yuhas A. J, and United States. National Aeronautics and Space Administration., eds. Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach. National Aeronautics and Space Administration, 1996.

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11

United States. National Aeronautics and Space Administration., ed. SRM internal flow test and computational fluid dynamic analyses: Final report, contract NAS8-39095. ERC, Inc., 1995.

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12

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

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13

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

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14

International Conference on Optical Methods and Data Processing in Heat and Fluid Flow (1998 London, England). International Conference on Optical Methods and Data Processing in Heat and Fluid Flow, 16-17 April 1998, London, UK. Professional Engineering Pub. for the Institution of Mechanical Engineers, 1998.

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15

United States. National Aeronautics and Space Administration., ed. A combined geometric approach for solving the Navier-Stokes equations on dynamic grids. National Aeronautics and Space Administration, 1995.

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16

United States. National Aeronautics and Space Administration., ed. A combined geometric approach for solving the Navier-Stokes equations on dynamic grids. National Aeronautics and Space Administration, 1995.

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17

United States. National Aeronautics and Space Administration., ed. SRM INTERNAL FLOW TESTS AND COMPUTATIONAL FLUID DYNAMIC FINAL REPORT... NASA-CR-203933... MAY 30, 1997. s.n., 1999.

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18

Center, Lewis Research. Surface modeling, grid generation, and related issues in computational fluid dynamic (CFD) solutions: Proceedings of a workshop sponsored by the NASA Steering Committee on Surface Modeling and Grid Generation and held at NASA Lewis Research Center, Cleveland, Ohio, May 9-11, 1995. Lewis Research Center, 1995.

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19

NASA Workshop on Surface Modeling, Grid Generation, and Related Issues in Computational Fluid Dynamics (CFD) Solutions (1995 NASA Lewis Research Center). Surface modeling, grid generation, and related issues in computational fluid dynamic (CFD) solutions: Proceedings of a workshop. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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20

United States. National Aeronautics and Space Administration., ed. SRM INTERNAL FLOW TESTS AND COMPUTATIONAL FLUID DYNAMIC ANALYSIS FINAL REPORT... NASA-CR-203931... SEP. 16, 1997. s.n., 1999.

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21

N, Duque Earl P., and United States. National Aeronautics and Space Administration., eds. Helicopter rotor blade computation in unsteady flows using moving overset grids. American Institute of Aeronautics and Astronautics, 1996.

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22

G, Chen, and United States. National Aeronautics and Space Administration., eds. A computational fluid dynamic and heat transfer model for gaseous core and gas cooled space power and propulsion reactors. National Aeronautics and Space Administration, 1996.

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23

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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24

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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26

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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27

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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28

El-Hady, Nabil M. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. Langley Research Center, 1993.

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29

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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30

United States. National Aeronautics and Space Administration., ed. A CFD/CSD interaction methodology for aircraft wings: A dissertation ... National Aeronautics and Space Administration, 1997.

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31

Krishnan, Sanjeev. Object-oriented implementation of the NAS parallel benchmarks using charm++: Annual report. National Aeronautics and Space Administration, 1996.

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32

Milind, Bhandarkar, Kalé Laxmikant Vasudeo, and United States. National Aeronautics and Space Administration., eds. Object-oriented implementation of the NAS parallel benchmarks using charm++: Annual report. National Aeronautics and Space Administration, 1996.

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33

United States. National Aeronautics and Space Administration., ed. Parallel NPARC: Implementation and performance. NYMA, Inc., 1996.

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34

R, Biswas, and United States. National Aeronautics and Space Administration., eds. Unstructured adaptive grid computations on an array of SMPs. Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

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35

Williams, R. W. Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion: Proceedings of a workshop held at NASA George C. Marshall Space Flight Center, Huntsville, Alabama, April 28-30, 1992. George C. Marshall Space Flight Center, 1992.

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36

Guruswamy, Guru P. User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1). National Aeronautics and Space Administration, Ames Research Center, 1994.

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37

Guruswamy, Guru P. User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1). National Aeronautics and Space Administration, Ames Research Center, 1994.

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38

Guruswamy, Guru P. User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1). National Aeronautics and Space Administration, Ames Research Center, 1994.

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39

Guruswamy, Guru P. User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1). National Aeronautics and Space Administration, Ames Research Center, 1994.

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40

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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41

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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42

Sumanta, Acharya, and Lewis Research Center, eds. Dynamics of large-scale structures for jets in crossflow. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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43

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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44

Center, Langley Research, ed. Summary report of the orbital X-34 wing static aeroelastic study. National Aeronautics and Science Administration, Langley Research Center, 2001.

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45

Center, Langley Research, ed. Summary report of the orbital X-34 wing static aeroelastic study. National Aeronautics and Science Administration, Langley Research Center, 2001.

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46

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

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47

Bernard, Guerts, Clercx H. J. H, and Uijttewaal Wim S. J, eds. Particle-laden flow: From geophysical to Kolmogorov scales. Springer, 2007.

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48

Maurice, Holt, Packard Andrew, and Institute for Computer Applications in Science and Engineering., eds. Simulation of a controlled airfoil with jets. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1997.

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49

Borri, Claudio, and Claudio Mannini, eds. Aeroelastic Phenomena and Pedestrian-Structure Dynamic Interaction on Non-Conventional Bridges and Footbridges. Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-6453-202-8.

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Abstract:
Fluid-structure and pedestrian-structure interaction phenomena are extremely important for non-conventional bridges. The results presented in this volume concern: simplified formulas for flutter assessment; innovative structural solutions to increase the aeroelastic stability of long-span bridges; numerical simulations of the flow around a benchmark rectangular cylinder; examples of designs of large structures assisted by wind-tunnel tests; analytical, computational and experimental investigation of the synchronisation mechanisms between pedestrians and footbridge structures. The present book is addressed to a wide audience including professionals, doctoral students and researchers, aiming to increase their know-how in the field of wind engineering, bluff-body aerodynamics and bridge dynamics.
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50

M, O'Farrell J., and George C. Marshall Space Flight Center., eds. High frequency flow/structural interaction in dense subsonic fluids. National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

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