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Libros sobre el tema "Composite PEKK"

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Autor: Grafiati
Publicado: 18 de mayo de 2024

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1

Ko, Henry Y. S. Reconsolidation pressure effects when healing delaminated thermoplastic composite structures. [Downsview, Ont.]: Dept. of Aerospace Studies and Engineering, 1989.

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2

Graves, Michael J. Initiation and extent of impact damage in graphite/epoxy and graphite/PEEK composites. New York: AIAA, 1988.

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3

Center, Langley Research y United States. Army Aviation Systems Command., eds. Mechanical property characterization and impact resistance of selected graphite/PEEK composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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4

1928-, Sun C. T. y Langley Research Center, eds. A constitutive model for AS4/PEEK thermoplastic composites under cyclic loading. West Lafayette, IN: Purdue University, School of Aeronautics and Astronautics, 1990.

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5

J, Magold N. y George C. Marshall Space Flight Center., eds. Cross-sectional examination of the damage zone in impacted specimens of carbon/epoxy and carbon/peek composites. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1990.

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6

J, Magold N. y George C. Marshall Space Flight Center., eds. Cross-sectional examination of the damage zone in impacted specimens of carbon/epoxy and carbon/peek composites. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1990.

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7

J, Magold N. y George C. Marshall Space Flight Center., eds. Cross-sectional examination of the damage zone in impacted specimens of carbon/epoxy and carbon/peek composites. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1990.

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8

Georgiou, I. Dissipation of mechanical work and temperature rise in AS4/PEEK thermoplastic composite. West Lafayette, Ind: Composite Materials Laboratory, Purdue University, School of Aeronautics and Astronautics, 1990.

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9

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. Boulder, Colo: U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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10

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. Boulder, Colo: U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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11

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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12

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. Boulder, Colo: U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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13

Rule, D. L. Low-temperature thermal conductivity of composites: Alumina fiber/epoxy and alumina fiber/PEEK. Boulder, Colo: U.S. Dept. of Commerce, National Bureau of Standards, 1989.

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14

Lloyd, John Richard. Thermal and mechanical properties of poly (ether ether ketone) (PEEK), and the carbon fibre composite APC-2. Birmingham: University of Birmingham, 1989.

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15

Mukasa, Victor. A comparison of the mechanical properties of composites made from braided and from undirectional carbon fibre reinforced "peek" prepreg. Manchester: UMIST, 1993.

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16

Characterization of mode I and mode II delamination growth and thresholds in graphite/peek composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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17

Strain rate dependent modeling of polymer matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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18

National Aeronautics and Space Administration (NASA) Staff. Constitutive Model for As4/Peek Thermoplastic Composites under Cyclic Loading. Independently Published, 2018.

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19

National Aeronautics and Space Administration (NASA) Staff. Characterization of Mode 1 and Mode 2 Delamination Growth and Thresholds in Graphite/Peek Composites. Independently Published, 2018.

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20

Narang, Gopi Chand. The Urdu Ghazal. Traducido por Surinder Deol. Oxford University Press, 2020. http://dx.doi.org/10.1093/oso/9780190120795.001.0001.

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The Urdu ghazal is a marvel of the magnetic dynamism of husn o i’shq filled with innovative imagery. It is a celebration of life and love in an ambiance of pure ecstasy. It has a profound capacity for joy as well as pain. It is the soul of Urdu verse and the play of creativity at its peak. No other poetic genre is as innately musical as the ghazal. The book presents unique flowering of the Urdu ghazal as a by-product of India’s composite culture that evolved from intermixing of Indian and foreign value systems. This never-before narrated story of the evolution of the Urdu ghazal is documented in eight chapters divided into three parts. It explores a variety of influences, including Sufism, Bhakti movement, and infusion of Rekhta and Persian languages and culture. The book explains classical ghazal forms that blossomed from the seeds sown by Amir Khusrau in the fourteenth century to great heights of literary excellence achieved during the next 300, notably in the works of great poets like Mir and Ghalib. Different socio-political and cultural demands of changing times are expounded towards the end, primarily how the ghazal provided new creative models to deal with literary movements like progressivism, modernism, and postmodernism. This book includes samples of works of thematically related poets. It also covers works of twentieth-century pioneering innovators like Firaq Gorakhpuri and Faiz Ahmed Faiz, and postmoderns like Gulzar and Javed Akhtar.
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