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1

Takanashi, Susumu. Large-scale numerical aerodynamic simulations for complete aircraft configurations. National Aerospace Laboratory, 1990.

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2

Meakin, Robert L. Unsteady aerodynamic simulations of multiple bodies in relative motion: A prototype method. National Aeronautics and Space Administration, Ames Research Center, 1990.

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3

N, Gupta Roop, Price Joseph M, and United States. National Aeronautics and Space Administration., eds. DSMC simulations of OREX entry conditions. National Aeronautics and Space Administration, 1996.

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4

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. American Institute of Aeronautics and Astronautics, 1998.

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5

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. American Institute of Aeronautics and Astronautics, 1998.

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6

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. American Institute of Aeronautics and Astronautics, 1998.

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7

Lawrence, C. Unsteady cascade aerodynamic response using a multiphysics simulation code. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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8

G, Potapczuk Mark, and Lewis Research Center, eds. Simulation of iced wing aerodynamics. NASA Lewis Research Center, 1991.

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9

G, Potapczuk Mark, and United States. National Aeronautics and Space Administration., eds. Simulation of iced wing aerodynamics. National Aeronautics and Space Administration, 1991.

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10

Center, NASA Glenn Research, ed. Aerodynamic simulation of ice accretion on airfoils. National Aeronautics and Space Administration, Glenn Research Center, 2011.

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11

Marvin, Joseph G. Progress and challenges in modeling turbulent aerodynamic flows. National Aeronautics and Space Administration, Ames Research Center, 1990.

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12

Foo, Lee, and Ames Research Center, eds. Numerical Aerodynamic Simulation Program Long Haul Communications Prototype. National Aeronautics and Space Administration, Ames Research Center, 1987.

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13

R, Reddy T. S., and United States. National Aeronautics and Space Administration., eds. Numerical simulations of supersonic flow through oscillating cascade sections. National Aeronautics and Space Administration, 1990.

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14

Barger, Raymond L. Semianalytic modeling of aerodynamic shapes. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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15

S, Rosen Bruce, ed. F-14A aircraft high-speed flow simulations. National Aeronautics and Space Administration, Langley Research Center, 1985.

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16

Center, Langley Research, ed. Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data. National Aeronautics and Space Administration, Langley Research Center, 1995.

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17

Messina, Michael D. Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data. National Aeronautics and Space Administration, Langley Research Center, 1995.

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18

Center, Ames Research, ed. Incompressible viscous flow simulations of the NFAC wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1986.

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19

Inouye, Mamoru. A decade of computer simulations for space shuttle aerodynamics. National Aeronautics and Space Administration, Ames Research Center, 1988.

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20

Snyder, Aaron. Numerical simulation of subsonic and transonic propeller flow. National Aeronautics and Space Administration, 1988.

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21

United States. National Aeronautics and Space Administration., ed. Numerical simulation of subsonic and transonic propeller flow. National Aeronautics and Space Administration, 1988.

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22

Srivastava, Rakesh. Simulation of unsteady rotational flow over propfan configuration. National Aeronautics and Space Administration, 1990.

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23

Srivastava, Rakesh. Simulation of unsteady rotational flow over propfan configuration. National Aeronautics and Space Administration, 1990.

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24

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Computer simulation of a wind tunnel test section with discrete finite-length wall slots. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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25

Hamed, A. Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems. National Aeronautics and Space Administration, 1989.

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26

Golovachov, Yuri P. Numerical simulation of viscous shock layer flows. Kluwer Academic Publishers, 1995.

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27

United States. National Aeronautics and Space Administration., ed. Direct numerical simulations of a temporally evolving mixing layer subject to forcing. National Aeronautics and Space Administration, 1987.

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28

D, Wieseman Carol, and Langley Research Center, eds. Time simulation of flutter with large stiffness changes. National Aeronautics and Space Administration, Langley Research Center, 1992.

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29

López Mejia, Omar Darío, and Jaime A. Escobar Gomez, eds. Numerical Simulation of the Aerodynamics of High-Lift Configurations. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-62136-4.

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30

Whatmough, Kenneth John. Aerodynamics, engine, and tire models for piloted flight simulation. National Library of Canada, 1994.

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31

Churchfield, Matthew J. A large-eddy simulation of wind-plant aerodynamics: Preprint. National Renewable Energy Laboratory, Office of Energy Efficiency and Renewable Energy, 2012.

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32

United States. National Aeronautics and Space Administration., ed. An overview of three approaches to multidisciplinary aeropropulsion simulations. National Aeronautics and Space Administration, 1997.

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33

1945-, Burns John A., and Langley Research Center, eds. A PDE sensitivity equation for optimal aerodynamic design. National Aeronautics and Space Administration, Langley Research Center, 1996.

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34

Bailey, Frank R. Status and projections of the NAS program. National Aeronautics and Space Administration, Ames Research Center, 1987.

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35

Center, Ames Research, ed. NAS technical summaries: Numerical Aerodynamic Simulation Program, March 1992-February 1993. National Aeronautics and Space Administration, Ames Research Center, 1994.

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36

Center, Ames Research, ed. NAS technical summaries: Numerical Aerodynamic Simulation Program, March 1989-February 1990. National Aeronautics and Space Administration, Ames Research Center, 1990.

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37

S, Chaussee D., Steger Joseph L, and Ames Research Center, eds. Numerical simulation of the hypersonic flow around lifting vehicles. National Aeronautics and Space Administration, Ames Research Center, 1987.

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38

S, Chaussee D., Steger Joseph L, and Ames Research Center, eds. Numerical simulation of the hypersonic flow around lifting vehicles. National Aeronautics and Space Administration, Ames Research Center, 1987.

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39

P, Friedmann Peretz, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.

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40

Peretz, Friedmann, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.

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41

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
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42

L, Haas Brian, and United States. National Aeronautics and Space Administration., eds. Particle kinetic simulation of high altitude hypervelocity flight. National Aeronautics and Space Administration, 1994.

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43

Center, Ames Research, ed. Particle kinetic simulation of high altitude hypervelocity flight. NASA National Aeronautics and Space Administration, Ames Research Center, 1994.

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44

E, Lawson Robert, and United States. Environmental Protection Agency., eds. Fluid modeling simulation of stack-tip downwash for neutrally buoyant plumes. U.S. Environmental Protection Agency, 1992.

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45

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Computational aerodynamics based on the Euler equations. AGARD, 1994.

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46

Krist, Steven E. Numerical simulation of channel flow transition: Resolution requirements and structure of the hairpin vortex. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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47

A, Zang Thomas, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Numerical simulation of channel flow transition: Resolution requirements and structure of the hairpin vortex. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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48

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. National Aeronautics and Space Administration, Langley Research Center, 1992.

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49

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. National Aeronautics and Space Administration, Langley Research Center, 1992.

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50

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. National Aeronautics and Space Administration, Langley Research Center, 1992.

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