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1

Jacobs, Peter A. Transient, hypervelocity flow in an axisymmetric nozzle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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2

Chandrasekhara, M. S. Compressibility effects on dynamic stall of airfoils undergoing rapid transient pitching motion. [Washington, DC: National Aeronautics and Space Administration, 1992.

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3

Chandrasekhara, M. S. Compressibility effects on dynamic stall of airfoils undergoing rapid transient pitching motion. [Washington, DC: National Aeronautics and Space Administration, 1992.

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4

Murthy, S. N. B. Transient performance of fan engine with water ingestion. [Washington, DC]: National Aeronautics and Space Administration, U.S. Dept. of Transportation, Federal Aviation Administration, 1993.

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5

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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6

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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7

Jacobs, Peter A. Numerical simulation of transient hypervelocity flow in an expansion tube. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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8

Schulte-Werning, Burkhard, Rémi Grégoire, Antonio Malfatti, and Gerd Matschke, eds. TRANSAERO — A European Initiative on Transient Aerodynamics for Railway System Optimisation. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-540-45854-8.

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9

Moore, F. K. A theory of post-stall transients in multistage axial compression systems. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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10

Forum on Unsteady Flow (4rd 1987 Boston, Mass.). Forum on Unsteady Flow - 1987: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Boston, Massachusetts, December 13-18, 1987. New York, N.Y. (345 E. 47th St., New York 10017): ASME, 1987.

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11

Unsteady transonic heat transfer in a transient facility: Semi-annual progress report. [Syracuse, N.Y.]: Syracuse University, Dept. of Mechanical and Aerospace Engineering, 1985.

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12

Gene, Hou, and United States. National Aeronautics and Space Administration., eds. Nonlinear transient thermal analysis by the force-derivative method: Final report for the period ending January 3, 1996. [Washington, DC: National Aeronautics and Space Administration, 1997.

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13

A, Bakhle Milind, and United States. National Aeronautics and Space Administration., eds. Cascade flutter analysis with transient response aerodynamics. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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14

United States. National Aeronautics and Space Administration., ed. Transient Ejector Analysis (TEA) code user's guide. [Washington, DC: National Aeronautics and Space Administration, 1993.

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15

Burkhard, Schulte-Werning, ed. TRANSAERO: A European initiative on transient aerodynamics for railway system optimisation. Berlin: Springer, 2002.

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16

Schulte-Werning, Burkhard, Remi Gregoire, Antonio Malfatti, and Gerd Matschke. TRANSAERO - A European Initiative on Transient Aerodynamics for Railway System Optimisation. Springer Berlin Heidelberg, 2010.

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17

M, Greitzer Edward, and Lewis Research Center, eds. A theory of post-stall transients in multistage axial compression systems. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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18

(Editor), Burkhard Schulte-Werning, Remi Gregoire (Editor), Antonio Malfatti (Editor), and Gerd Matschke (Editor), eds. TRANSAERO A European Initiative on Transient Aerodynamics for Railway System Optimization (Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)). Springer, 2002.

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19

A, Schroeder Jeffery, Ames Research Center, and United States. Army Aviation Research and Technology Activity., eds. An investigation of the ability to recover from transients following failures for single-pilot rotorcraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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20

A, Schroeder Jeffery, Ames Research Center, and United States. Army Aviation Research and Technology Activity., eds. An investigation of the ability to recover from transients following failures for single-pilot rotorcraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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