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1

United States. National Aeronautics and Space Administration., a cura di. Eno-Oshers schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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2

United States. National Aeronautics and Space Administration., a cura di. Eno-Oshers schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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3

United States. National Aeronautics and Space Administration., a cura di. Eno-Osher schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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4

Huynh, Hung T. Accurate upwind methods for the Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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5

Fuhrer, Claus. Formulation and numerical solution of the equations of constrained mechanical motion. Koln: DFLVR, 1989.

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6

Ajay, Kumar, e Langley Research Center, a cura di. Compact high order schemes for the Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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7

Center, Langley Research, a cura di. Singularities of the Euler equation and hydrodynamic stability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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8

E, Turkel, e United States. National Aeronautics and Space Administration., a cura di. Central difference TVD and TVB schemes for time dependent and steady state problems. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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9

Center, Langley Research, a cura di. Singularities of the Euler equation and hydrodynamic stability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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10

M, Atassi H., e United States. National Aeronautics and Space Administration., a cura di. Numerical solutions of the linearized Euler equations for unsteady vortical flows around lifting airfoils. [Washington, DC: National Aeronautics and Space Administration, 1990.

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11

R, Chakravarthy Sukumar, e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., a cura di. A user guide for the EMTAC-MZ CFD code. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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12

Walters, Robert W. Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions. [Washington, DC]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1987.

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13

Walters, Robert W. Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions. [Washington, DC]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1987.

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14

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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15

Chen, Robert T. N. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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16

Center, Ames Research, a cura di. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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17

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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18

E, Turkel, Schaffer Steve e United States. National Aeronautics and Space Administration., a cura di. Comparison of three explicit multigrimethods for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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19

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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20

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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21

Air Resources Laboratory (U.S.), a cura di. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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22

Center, Ames Research, a cura di. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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23

Center, Ames Research, a cura di. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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24

Center, Langley Research, a cura di. A numerical resolution study of high order essentially non-oscillatory schemes applied to recompressible flow. Hampton, Va: ICASE, National Aeronautics and Space Administration, Langley Research Center, 1992.

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25

Center, Ames Research, a cura di. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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26

Center, Ames Research, a cura di. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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27

Chen, Robert T. N. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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28

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

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29

Milev, Ivo. Integrierte Modelle zur physikalischen Interpretation geodatischer Deformationsuntersuchungen. Munchen: Verlag der Bayerischen Akademie der WissenschaftKommission bei der C.H. Beck'schen Verlagsbuchhandlung, 2001.

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30

Center, Ames Research, a cura di. Solution of nonlinear flow equations for complex aerodynamic shapes. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1992.

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31

Center, Ames Research, a cura di. Solution of nonlinear flow equations for complex aerodynamic shapes. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1992.

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32

Bennett, Andrew F. Lagrangian fluid dynamics. Cambridge: Cambridge University Press, 2005.

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33

Sporykhin, A. N. Kombinirovannyĭ podkhod Ėĭlera-Lagranzha v mekhanike sploshnoĭ sredy. Voronezh: Izd-vo Voronezhskogo universiteta, 1991.

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34

Kumar, Jain Romesh, a cura di. Solution of two-dimensional Euler equations: Experience with a finite volume code. Köln: DFVLR, 1987.

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35

Center, Langley Research, a cura di. Canonical forms of multidimensional steady inviscid flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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36

United States. National Aeronautics and Space Administration., a cura di. Structural optimization of large structural systems by optimality criteria methods. [Washington, DC: National Aeronautics and Space Administration, 1992.

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37

X, Ying S., Ames Research Center e United States. Army Aviation Systems Command. Army Aviation Research and Technology Activity., a cura di. Euler solution of multiblade rotor flow. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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38

Meĭrmanov, A. M. Evolution equations and Lagrangian coordinates. Berlin: Walter de Gruyter, 1997.

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39

Dehn, Edgar. Algebraic equations: An introduction to the theories of Lagrange and Galois. Mineola, N.Y: Dover Publications, 2004.

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40

Center, Langley Research, a cura di. Three dimensional unstructured multigrid for the Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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41

J, Mavriplis D., e Langley Research Center, a cura di. Agglomeration multigrid for the three-dimensional Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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42

Anderson, W. Kyle. Accurate solutions, parameter studies, and comparisons for the Euler and potential flow equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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43

McDonald, Aidan. The origin of noise in semi-Lagrangian integrations. Dublin: Met Éireann, 1998.

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44

Posiadała, Bogdan. Modelowanie i analiza drgań ciągło-dyskretnych układów mechanicznych: Zastosowanie formalizmu mnożników Lagrange'a. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2007.

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45

Jentink, Thomas Neil. Formulation of boundary conditions for the multigrid acceleration of the Euler and Navier Stokes equations. West Lafayette, Ind: Purdue University, School of Aeronautics and Astronautics, 1990.

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46

INRIA Workshop on Numerical Methods for the Euler Equations of Fluid Dynamics (1983 Rocquencourt, Yvelines, France). Numerical methods for the Euler equations of fluid dynamics. Philadelphia: Society for Industrial and Applied Mathematics, 1985.

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47

Șandru, Ovidiu-Ilie. Local Hamilton-Lagrange structures: Applications in the partial differential equations theory. Timișoara: Universitatea din Timișoara, Facultatea de Matematică, 1994.

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48

Rossow, Cord-Christian. Berechnung von Strömungsfeldern durch Lösung der Euler-Gleichungen mit einer erweiterten Finite-Volumen Diskretisierungsmethode. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1989.

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49

L, Van Dommelen Leon, Lam Shui T e Langley Research Center, a cura di. On the use of Lagrangian variables in descriptions of unsteady boundary-layer separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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50

Giachetta, G. Advanced classical field theory. Hackensack, NJ: World Scientific, 2009.

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