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Libros sobre el tema "Shear panel"

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Autor: Grafiati
Publicado: 14 de marzo de 2023

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1

Ko, William L. Shear buckling analysis of a hat-stiffened panel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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2

Kianoush, Mohammed Reza. Inelastic seismic response of precast concrete large panel coupled shear wall systems. [Regina]: Dept. of Civil Engineering, University of Alberta, 1986.

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3

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel., ed. Fluid dynamics of three-dimensional turbulent shear flows and transition: Papers presented and discussions held at the Symposium of the FluidDynamics Panel in Cesme, Turkey, 3-6 October 1988. Neuilly sur Seine: Agard, 1989.

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4

Hanhijarvi, Antti. Computational optimisation of test specimen for planar shear strength tests of wood based panels. Espoo, Finland: VTT, Technical Research Centre of Finland, 1998.

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5

Larry, Sobel y Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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6

Larry, Sobel y Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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7

Ko, William L. Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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8

F, Knight Norman, Reddy J. N. 1945- y Langley Research Center, eds. Interlaminar shear stress effects on the postbuckling response of graphite-epoxy panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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9

Ko, William L. Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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10

Farley, Gary L. Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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11

Farley, Gary L. Effect of low-velocity or ballistic impact damage on the strength of thin composite and aluminum shear panels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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12

Crawford, Laura y Ruth Kleinpell. Principles and prevention of pressure sores in the ICU. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199600830.003.0279.

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A pressure ulcer, defined by the National Pressure Advisory Panel and European Pressure Ulcer Advisory Panels as localized injury to the skin or tissue as the result of pressure or pressure in combination with shear, can be an adverse complication of a hospital stay, especially for acute and critically-ill patients. Factors that can contribute to pressure ulcer development include the intensity and duration of pressure, tissue tolerance, shear, and friction. Common anatomical sites for pressure ulcers development are over bony prominences. The National Pressure Advisory Panel and European Pressure Ulcer Advisory Panels define pressure ulcers in six stages according to the degree of tissue damage present in the wound. A risk assessment should be performed to identify the vulnerability of pressure ulcer development and provide guidance for the implementation of preventative interventions. For the critically-ill patient, several specific measures are advocated for preventing pressure ulcers.
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13

Progressive failure studies of stiffened panels subjected to shear loading. Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, ICASE, 2002.

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14

National Aeronautics and Space Administration (NASA) Staff. Progressive Failure Studies of Stiffened Panels Subjected to Shear Loading. Independently Published, 2018.

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15

Ford, Ford Madox. The Panel: A Sheer Comedy (Collected Works of Ford Madox Ford). Classic Books, 2000.

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16

Relationship between voids and interlaminar shear strength of polymer matrix composites. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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17

National Aeronautics and Space Administration (NASA) Staff. Novel Composites for Wing and Fuselage Applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear. Independently Published, 2018.

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