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1

Guoying, Zhao. Nonequilibrium phenomena behind a bow shock wave in a dusty gas. [S.l.]: [s.n.], 1985.

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2

United States. National Aeronautics and Space Administration., ed. ICE/ISEE plasma wave data analysis: Final report for period January 1992-September 1993. Redondo Beach, Calif: TRW Space And Technology Group, Applied Technology Division, 1993.

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3

United States. National Aeronautics and Space Administration., ed. ICE/ISEE plasma wave data analysis: Final report for period January 1990-December 1991. Redondo Beach, Calif: TRW Space And Technlogy Group, Applied Technology Division, 1992.

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4

Grabbe, Crockett L. Analytical MHD theory for Earth's bow shock at low Mach numbers. [Washington, DC: National Aeronautics and Space Administration, 1995.

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5

L, Grabbe Crockett, and United States. National Aeronautics and Space Administration., eds. Towards an MHD theory for the standoff distance of earth's bow shock. [Washington, DC: National Aeronautics and Space Administration, 1997.

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6

Ahuja, J. K. Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique. Washington, D. C: American Institute of Aeronautics and Astronautiacs, 1994.

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7

B, Hospodarsky G., and United States. National Aeronautics and Space Administration., eds. The fine structure of Langmuir waves observed upstream of the bow shock at Venus. Iowa City, Iowa: Dept. of Physics and Astronomy, The University of Iowa, 1994.

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8

J, Singh D., Tiwari S. N, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique: Progress report for the period ended June 30, 1994. Norfolk, Va: Old Dominion University Research Foundation, 1994.

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9

J, Capone Francis, and Langley Research Center, eds. Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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10

Homayoun, Karimabadi, Krauss-Varban Dietmar, and United States. National Aeronautics and Space Administration., eds. Physics of boundaries and their interactions in space plasmas: Interim contractor report #32 (final), 6/01/99-6/30/99. San Diego, CA: SciberNet, Inc., 1999.

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11

Homayoun, Karimabadi, Krauss-Varban Dietmar, and United States. National Aeronautics and Space Administration., eds. Physics of boundaries and their interactions in space plasmas: Interim contractor report #32 (final), 6/01/99-6/30/99. San Diego, CA: SciberNet, Inc., 1999.

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12

Homayoun, Karimabadi, Krauss-Varban Dietmar, and United States. National Aeronautics and Space Administration., eds. Physics of boundaries and their interactions in space plasmas: Final contractor report #19, 5/01/98-5/31/98. San Diego, CA: SciberNet, Inc., 1998.

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13

Homayoun, Karimabadi, Krauss-Varban Dietmar, and United States. National Aeronautics and Space Administration., eds. Physics of boundaries and their interactions in space plasmas: Final contractor report #19, 5/01/98-5/31/98. San Diego, CA: SciberNet, Inc., 1998.

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14

Eberhard, Möbius, Lee Martin A, and United States. National Aeronautics and Space Administration., eds. Particle acceleration and transport in the tail and at the front side of the Magnetosphere: Final report, NASA grant NAG5-1548. [Washington, DC: National Aeronautics and Space Administration, 1994.

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15

Eberhard, Möbius, Lee Martin A, and United States. National Aeronautics and Space Administration., eds. Particle acceleration and transport in the tail and at the front side of the Magnetosphere: Final report, NASA grant NAG5-1548. [Washington, DC: National Aeronautics and Space Administration, 1994.

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16

United States. National Aeronautics and Space Administration., ed. Final report on Venus data analysis program grant number NAGW-3497, "Plasma waves in the magnetosheath of Venus". [Washington, DC: National Aeronautics and Space Administration, 1996.

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17

Displacement of the Earth's Bow Shock and Magnetopause Due to an Impinging Interplanetary Shock Wave. Storming Media, 1997.

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18

National Aeronautics and Space Administration (NASA) Staff. Fine Structure of Langmuir Waves Observed Upstream of the Bow Shock at Venus. Independently Published, 2018.

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19

Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique: Progress report for the period ended June 30, 1994. Norfolk, Va: Old Dominion University Research Foundation, 1994.

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20

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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21

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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22

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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