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Libros sobre el tema "Flutter Stability"

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Autor: Grafiati
Publicado: 6 de septiembre de 2023

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1

Woods, Jessica A. Results of a parametric aeroelastic stability analysis of a generic x-wing aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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2

NASA Dryden Flight Research Center., ed. A historical overview of flight flutter testing. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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3

1945-, Bennett Robert M. y Langley Research Center, eds. Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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4

United States. National Aeronautics and Space Administration, ed. Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corp., 1986.

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5

United States. National Aeronautics and Space Administration., ed. Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corp., 1986.

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6

United States. National Aeronautics and Space Administration., ed. FPCAS3D user's guide: Full potential aeroelastic program. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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7

United States. National Aeronautics and Space Administration., ed. FPCAS3D user's guide: Full potential aeroelastic program. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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8

United States. National Aeronautics and Space Administration., ed. Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls. [Alexandria, Va.]: American Helicopter Society, 1991.

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9

Nissim, E. Effect of control surface mass unbalance on the stability of a closed-loop active control system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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10

Borri, Claudio y Claudio Mannini, eds. Aeroelastic Phenomena and Pedestrian-Structure Dynamic Interaction on Non-Conventional Bridges and Footbridges. Florence: Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-6453-202-8.

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Resumen
Fluid-structure and pedestrian-structure interaction phenomena are extremely important for non-conventional bridges. The results presented in this volume concern: simplified formulas for flutter assessment; innovative structural solutions to increase the aeroelastic stability of long-span bridges; numerical simulations of the flow around a benchmark rectangular cylinder; examples of designs of large structures assisted by wind-tunnel tests; analytical, computational and experimental investigation of the synchronisation mechanisms between pedestrians and footbridge structures. The present book is addressed to a wide audience including professionals, doctoral students and researchers, aiming to increase their know-how in the field of wind engineering, bluff-body aerodynamics and bridge dynamics.
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11

Multifunction tests of a frequency domain based flutter suppression system. Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, 1992.

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12

National Aeronautics and Space Administration (NASA) Staff. Rotor Design Options for Improving XV-15 Whirl-Flutter Stability Margins. Independently Published, 2018.

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13

The effect of steady aerodynamic loading on the flutter stability of turbomachinery blading. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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14

ASTROP2 users manual: A program for aeroelastic stability analysis of propfans. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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15

Response of the alliance 1 proof-of-concept airplane under gust loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.

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