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1

Yeffet, Amir. A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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2

Yeffet, Amir. A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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3

Yeffet, Amir. A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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4

Yeffet, Amir. A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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5

Yeffet, Amir. A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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6

Roe, P. L. Linear bicharacteristic schemes without dissipation. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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7

Institute for Computer Applications in Science and Engineering., ed. Linear bicharacteristic schemes without dissipation. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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8

R, Radespiel, Turkel E, and Institute for Computer Applications in Science and Engineering., eds. Comparison of several dissipation algorithms for central difference schemes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1997.

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9

Swanson, R. Charles. On central-difference and upwind schemes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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10

Swanson, R. Charles. On central-difference and upwind schemes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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11

Swanson, R. Charles. On central-difference and upwind schemes. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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12

Swanson, R. Charles. On central-difference and upwind schemes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1990.

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13

Hu, F. Q. Low-dissipation and -disperson Runge-Kutta schemes for computational acoustics. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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14

Yousuff, Hussaini M., Manthey J, and Institute for Computer Applications in Science and Engineering., eds. Low-dissipation and -disperson Runge-Kutta schemes for computational acoustics. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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15

C, Yee H., and Research Institute for Advanced Computer Science (U.S.), eds. Performance of low dissipative high order shock-capturing schemes for shock-turbulence interactions. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

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16

E, Turkel, and Langley Research Center, eds. Artificial dissipation and central difference schemes for the Euler and Navier-Stokes equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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17

United States. National Aeronautics and Space Administration., ed. Performance Of Low Dissipative High Order Shock-Capturing Schemes For Shock-Turbulence... NASA/CR-1998-208354... Aug. 6, 1998. [S.l: s.n., 1999.

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18

Brodersen, Olaf. Untersuchung einer Matrix-Dissipation in einem Zelleneckpunkt-Finite-Volumen-Schema zur Lösung der Navier-Stokes-Gleichungen. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1992.

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19

Low dissipative high order shock-capturing methods using characteristic-based filters. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

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20

National Aeronautics and Space Administration (NASA) Staff. Comparison of Several Dissipation Algorithms for Central Difference Schemes. Independently Published, 2018.

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21

Low-dissipation and -disperson Runge-Kutta schemes for computational acoustics. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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