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Bibliographies thématiques / LOAD DEFORMATION / Livres

Livres sur le sujet « LOAD DEFORMATION »

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Auteur : Grafiati

Publié le 11 septembre 2023

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1

M, Bahm Catherine, Heinle Robert A et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. Determination of stores pointing error due to wing flexibility under flight load. [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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2

Moskalenko, Vladislav, Ivan Druz', Lev Leont'ev et Valenin Tarasov. Features of the influence of the connection points of the set on the bearing capacity of the side floors of ice navigation vessels. ru : INFRA-M Academic Publishing LLC., 2022. http://dx.doi.org/10.12737/1870592.

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The monograph is devoted to the consideration of the problems of damage to the side floors of ice navigation vessels from the action of concentrated ice load. The problems of the ultimate equilibrium of the beams of the on-board set are solved, taking into account the features of the ladder fastening. Extensive model experiments on the supercritical deformation of beams are presented. The methods of designing and defecation of the on-board set of ice navigation vessels, taking into account the cable connections, are proposed. It can be useful to scientists, specialists of ship repair plants, senior students of maritime universities, as well as specialists of research institutes and design bureaus evaluating the structural safety of ships under the influence of ice load.

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3

S, Majumdar Bhaskar, et United States. National Aeronautics and Space Administration., dir. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC] : National Aeronautics and Space Administration, 1995.

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4

S, Majumdar Bhaskar, et United States. National Aeronautics and Space Administration., dir. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC] : National Aeronautics and Space Administration, 1995.

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5

S, Majumdar Bhaskar, et United States. National Aeronautics and Space Administration., dir. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC] : National Aeronautics and Space Administration, 1995.

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6

Sreeramesh, Kalluri, Bonacuse Peter J. 1960- et Symposium on Multiaxial Fatigue and Deformation : Testing and Prediction (1999 : Seattle, Wash.), dir. Multiaxial fatigue and deformation : Testing and prediction. W. Conshohocken, PA : ASTM, 2000.

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7

Eberhardshtayner, Yozef, Sergey Leonovich et Valentin Dorkin. Design models of structural building materials under multiaxial stress. ru : INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1082947.

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The monograph presents the results of experimental and theoretical studies of the behavior of wood and concrete of various structures under biaxial and triaxial compression. It contains a systematic classification of existing models for concrete that link three-axis nonlinear elastic stresses and deformations, as well as research and subsequent evaluation of some basic models from the point of view of their possible use in the framework of spatial load analysis using FEM. It is intended for scientific and engineering workers of research and design organizations.

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8

United States. National Aeronautics and Space Administration., dir. Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects. Bethesda, MD : Carderock Division, Naval Surface Warfare Center, 1993.

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9

Hyer, M. W. Innovative design of composite structures : Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. Blacksburg, Va : College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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10

Madenci, Erdogan. Implementation of free-formulation-based flat shell elements into NASA comet code and development of nonlinear shallow shell element : Grant NAG1-1626. [Hampton, Va.] : NASA Langley Research Center, 1997.

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11

Center, Langley Research, et United States. National Aeronautics and Space Administration., dir. Implementation of free-formulation-based flat shell elements into NASA comet code and development of nonlinear shallow shell element : Grant NAG1-1626. [Hampton, Va.] : NASA Langley Research Center, 1997.

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12

Center, Langley Research, et United States. National Aeronautics and Space Administration., dir. Implementation of free-formulation-based flat shell elements into NASA comet code and development of nonlinear shallow shell element : Grant NAG1-1626. [Hampton, Va.] : NASA Langley Research Center, 1997.

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13

Chudek, Mirosław. Loads and stress occuring in the orogen, in the vicinity of wall headings, remains of coal seams, and barrier pillars in underground mines. Wrocław : Zakład Narodowy im. Ossolińskich, 1985.

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14

Center, Langley Research, dir. An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.

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15

Center, Langley Research, dir. An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.

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16

Pramote, Dechaumphai, Thornton Earl A. 1936- et Langley Research Center, dir. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va : NASA Langley Research Center, 1990.

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17

Pandey, Ajay K. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va : NASA Langley Research Center, 1990.

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18

Pramote, Dechaumphai, Thornton Earl A. 1936- et Langley Research Center, dir. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va : NASA Langley Research Center, 1990.

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19

Pramote, Dechaumphai, Thornton Earl A. 1936- et Langley Research Center, dir. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va : NASA Langley Research Center, 1990.

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20

Test Methods for Deformation of Plastics Under Load (D621). Astm Intl, 1988.

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21

Abert, Benjamin. 22FTM16, a Model for Considering Wheel Body Deformation in Tooth Contact Load Distribution. American Gear Manufacturers Association, 2022.

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22

Response : A program to determine the load-deformation response of reinforced concrete sections. Ottawa : National Library of Canada, 1990.

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23

W, Venkata Ramana, et Bhabha Atomic Research Centre, dir. Effect of deformation on unloading compliance values of TPB specimens and throughwall circumferentially cracked straight pipes under four point bending load. Mumbai : Bhabha Atomic Research Centre, 2002.

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24

Donal, Erwan, Seisyou Kou et Partho Senguptadd. Left ventricle : cardiac mechanics and left ventricular performance. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780198726012.003.0019.

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The complexity of left ventricular (LV) function(s) assessment in heart failure patients is related to the complexity of heart anatomy, but also to the complexity of electromechanical interaction, and to the load dependency of all the parameters that could be applied in clinical practice. Three perpendicular axes orienting the global geometry of the LV define the local cardiac coordinate system: radial, circumferential, and longitudinal. Speckle tracking is the technique of choice for quantifying myocardial deformation (regional and global). Longitudinal LV deformation, which is predominantly governed by the subendocardial region, is the most vulnerable component of LV mechanics and therefore most sensitive to the presence of myocardial disease.

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25

Lindholm, Ulric S. Mechanical Behavior of Materials under Dynamic Loads. Springer, 2012.

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26

Implementation of free-formulation-based flat shell elements into NASA comet code and development of nonlinear shallow shell element : Grant NAG1-1626. [Hampton, Va.] : NASA Langley Research Center, 1997.

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27

An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.

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28

Mostafaei, Hossein. Axial-shear-flexure interaction approach for displacement-based evaluation of reinforced concrete elements = : Mage-sendan jukuryoku sōgo sayō moderu ni yoru tekkin konkurīto buzai no henkei seinō hyōka. 2006.

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