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1

Holdeman, J. D. Mixing of multiple jets with a confined subsonic crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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2

John, D. St. Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure. [Washington, D.C.]: National Aeronautics and Space Administration STI Preogram Office, 2000.

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3

B, Lakshminarayana, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Three dimensional viscous flow field in an axial flow turbine nozzle passage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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4

Inc, OTT Engineering, ed. Inexpensive cross-flow hydropower turbine at the Arbuckle Mountain hydroelectric project (Reports). U.S. Dept. of Energy, Idaho Field Office., 1991.

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5

Experimental study of cross flow mixing in cylindrical and rectangular ducts. [Washington, DC: National Aeronautics and Space Administration, 1993.

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6

Center, Lewis Research, ed. Mixing of multiple jets with a confined subsonic crossflow: Summary of NASA-supported experiments and modeling. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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7

A, Cyr M., Strange R. R, and United States. National Aeronautics and Space Administration., eds. Turbine blade and vane heat flux sensor development phase 2. [Washington, DC]: National Aeronautics and Space Administration, 1985.

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8

D, Holdeman J., Samuelsen G. S, and Lewis Research Center, eds. Optimization of jet mixing into a rich, reacting crossflow. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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9

E, Smith C., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing and emission characteristics of transverse jets in annular and cylindrical confined crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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10

S, Samuelsen G., and United States. National Aeronautics and Space Administration., eds. Quick-mixing studies under reacting conditions: Under grant NAG3-1110. [Washington, DC: National Aeronautics and Space Administration, 1996.

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11

Quick-mixing studies under reacting conditions: Under grant NAG3-1110. [Washington, DC: National Aeronautics and Space Administration, 1996.

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12

S, Samuelsen G., and United States. National Aeronautics and Space Administration., eds. Quick-mixing studies under reacting conditions: Under grant NAG3-1110. [Washington, DC: National Aeronautics and Space Administration, 1996.

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13

S, Samuelsen G., and United States. National Aeronautics and Space Administration., eds. Quick-mixing studies under reacting conditions: Under grant NAG3-1110. [Washington, DC: National Aeronautics and Space Administration, 1996.

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14

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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15

Sumanta, Acharya, and Lewis Research Center, eds. Dynamics of large-scale structures for jets in crossflow. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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16

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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17

Sumanta, Acharya, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. Dynamics of large-scale structures for jets in crossflow. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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18

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Mixing of pure air jets with a reacting fuel-rich crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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19

S, Samuelsen G., and NASA Glenn Research Center, eds. Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2000.

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20

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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21

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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22

S, Samuelsen G., and United States. National Aeronautics and Space Administration., eds. Atomization and dispersion of a liquid jet injected into a crossflow of air: Under grant NAG3-1124. [Washington, DC: National Aeronautics and Space Administration, 1996.

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