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1

Gelder, Thomas F. Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel. Lewis Research Center, 1987.

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2

Ross, James C. Prediction of vortex-induced loads on wind tunnel turning vanes. National Aeronautics and Space Administration, Ames Research Center, 1985.

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3

Center, Ames Research, ed. Prediction of vortex-induced loads on wind tunnel turning vanes. National Aeronautics and Space Administration, Ames Research Center, 1985.

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4

Ross, James C. Prediction of vortex-induced loads on wind tunnel turning vanes. National Aeronautics and Space Administration, Ames Research Center, 1985.

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5

Moore, Royce D. Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. Lewis Research Center, 1987.

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6

G, Seasholtz Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Laser anemometer measurements and computations in an annular cascade of high turning core turbine vanes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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7

Johnson, Steven A. Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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8

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Laser anemometer measurements and computations for transonic flow conditions in an annular cascade of high turning core turbine vanes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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9

D, Moore Royce, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Researach Center's proposed altitude wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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10

Boldman, Donald R. Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. Lewis Research Center, 1987.

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11

R, Boldman Donald, Shyne Rickey J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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12

Wind tunnel turning vanes of modern design. National Aeronautics and Space Administration, 1985.

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13

Unsteady aerodynamic load estimates on turning vanes in the National Full-Scale Aerodynamic Complex. National Aeronautics and Space Administration, Ames Research Center, 1987.

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14

National Aeronautics and Space Administration (NASA) Staff. Laser Anemometer Measurements and Computations in an Annular Cascade of High Turning Core Turbine Vanes. Independently Published, 2018.

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15

National Aeronautics and Space Administration (NASA) Staff. Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes. Independently Published, 2018.

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16

Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Researach Center's proposed altitude wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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17

Woodturning: Bowls, platters, hollow forms, vases, vessels, bottles, flasks, tankards, plates. Guild of Master Craftsman Publications, 1999.

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18

Experimental evaluation of two turning vane designs for fan drive corner 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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19

Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.

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