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1

Meng-Sing, Liou, and United States. National Aeronautics and Space Administration., eds. A flux splitting scheme with high-resolution and robustness for discontinuities. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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2

Dochan, Kwak, and Ames Research Center, eds. An upwind-differencing scheme for the incompressible Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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3

Dochan, Kwak, and Ames Research Center, eds. An upwind-differencing scheme for the incompressible Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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4

Institute for Computer Applications in Science and Engineering., ed. Gas evolution dynamics in Godunov-type schemes and analysis of numerical shock instability. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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5

Institute for Computer Applications in Science and Engineering., ed. Gas evolution dynamics in Godunov-type schemes and analysis of numerical shock instability. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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6

Center, NASA Glenn Research, ed. Ten years in the making: AUSM-family. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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7

S, Liou M., and United States. National Aeronautics and Space Administration., eds. Hybrid upwind splitting (HUS) by a field-by-field decomposition. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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8

Lui, Shiu-Hong. Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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9

Roberto, Marsilio, and Institute for Computer Applications in Science and Engineering., eds. A numerical method for solving the three-dimensional parabolized Navier-Stokes equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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10

A new flux splitting scheme. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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11

An upwind-differencing scheme for the incompressible Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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12

Application of a third order upwind scheme to viscous flow over clean and iced wings: 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.

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13

Vabishchevich, Petr N. Additive Operator-Difference Schemes: Splitting Schemes. de Gruyter GmbH, Walter, 2013.

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14

Vabishchevich, Petr N. Additive Operator-Difference Schemes: Splitting Schemes. De Gruyter, Inc., 2013.

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15

Additive Operator-Difference Schemes: Splitting Schemes. De Gruyter, Inc., 2013.

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16

Additive operator-difference schemes: Splitting schemes. Berlin: Walter de Gruyter GmbH & Co. KG, 2014.

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17

Britain, Great. Registered Pension Schemes (Splitting of Schemes) Regulations 2006. Stationery Office, The, 2006.

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18

Britain, Great. Registered Pension Schemes (Splitting of Schemes) (Amendment) Regulations 2015. Stationery Office, The, 2015.

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19

Britain, Great. Registered Pension Schemes (Splitting of Schemes) (Amendment) Regulations 2007. Stationery Office, The, 2007.

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20

Hybrid upwind splitting (HUS) by a field-by-field decomposition. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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21

Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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22

A numerical method for solving the three-dimensional parabolized Navier-Stokes equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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