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Academic literature on the topic 'SHAPE OF TUNNEL'

Author: Grafiati
Published: 11 September 2023

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Books on the topic "SHAPE OF TUNNEL"

1

W, Moses Robert, and Langley Research Center, eds. A feasibility study to control airfoil shape using THUNDER. National Aeronautics and Space Administration, Langley Research Center, 1997.

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2

Mario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. National Aeronautics and Space Administration, 1995.

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3

Mario, Vargas Meza, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. National Aeronautics and Space Administration, 1995.

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4

Mario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. National Aeronautics and Space Administration, 1995.

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5

Mario, Vargas, and United States. National Aeronautics and Space Administration., eds. A laser-based ice shape profilometer for use in icing wind tunnels. National Aeronautics and Space Administration, 1995.

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6

M, Berkowitz Brian, and United States. National Aeronautics and Space Administration., eds. Experimental ice shape and performance characteristics for a multi-element airfoil in the NASA Lewis Icing Research Tunnel. National Aeronautics and Space Administration, 1991.

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7

J, Simoneau Robert, Ching Chang Y, and United States. National Aeronautics and Space Administration., eds. Influence of turbulence parameters, Reynolds number, and body shape on stagnation-region heat transfer. National Aeronautics and Space Administration, 1994.

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8

Cook, M. Systems tunnel linear shaped charge lightning strike: Final test report. Thiokol Corp., Space Operations, 1989.

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9

Randall, Peterson, and Ames Research Center, eds. Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1994.

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10

L, Peterson Randall, and Ames Research Center, eds. Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1994.

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