Books on the topic 'Fiber element method'

Mital, Subodh K. Fiber pushout test: A three-dimensional finite element computational simulation. [Washington, D.C.]: NASA, 1990.

Smith, Joseph-Aime Jean. Evaluation of three dimensional thermal stresses in laminated plates using pseudo three dimensional finite elements. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, 1985.

Naik, Rajiv A. Fracture mechanics analysis for various fiber/matrix interface loadings. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Gotsis, Pascal K. Progressive fracture of fiber composite build-up structures. [Washington, D.C: National Aeronautics and Space Administration, 1997.

Chamis, C. C. Computational simulation of structural fracture in fiber composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Ko, William L. Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Melis, Matthew E. COMGEN, a computer program for generating finite element models of composite materials at the micro level. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Koshiba, Masanori. Optical waveguide theory by the finite element method. Tokyo: KTK Scientific, 1993.

ZnO bao mo zhi bei ji qi guang, dian xing neng yan jiu. Shanghai Shi: Shanghai da xue chu ban she, 2010.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Elastic-plastic finite element analyses of an unidirectional, 9 vol % tungsten fiber reinforced copper matrix composite. [Washington, DC: National Aeronautics and Space Administration, 1993.

M, Arnold S., and NASA Glenn Research Center, eds. The applicability of the generalized method of cells for analyzing discontinuously reinforced composites. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

N, Murthy P. L., and United States. National Aeronautics and Space Administration., eds. Computational simulation of structural fracture in fiber composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Thermal analysis of a functionally graded material subject to a thermal gradient using the boundary element method. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. On the finite element implementation of the generalized method of cells micromechanics constitutive model. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Micromechanical Study of Interface Stress in a Fiber-Reinforced Composite under Transverse Loading Using Boundary Element Method. Storming Media, 2000.

Wang, Min. Three-dimensional, nonlinear viscoelastic analysis of laminated composites: A finite element approach. 1993.

Wang, Min. Three-dimensional, nonlinear viscoelastic analysis of laminated composites: A finite element approach. 1993.

M, Arnold S., Iyer Saiganesh K, and Lewis Research Center, eds. Flow/damage surfaces for fiber-reinforced metals having different periodic microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates. College Station, Tex: Center for Mechanics of Composites, Texas A&M University, 1990.

United States. National Aeronautics and Space Administration., ed. COMGEN, a computer program for generating finite element models of composite materials at the micro level. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

C, Chamis C., and Lewis Research Center, eds. Interlaminar fracture toughness: Three-dimensional finite-element modeling for end-notch and mixed-mode flexure. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

E, Harris Charles, and United States. National Aeronautics and Space Administration., eds. Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue. [Washington, D.C: National Aeronautics and Space Administration, 1995.

L, Bradley Walter, and United States. National Aeronautics and Space Administration., eds. Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates: An annual progress report. College Station, Tex: Center for Mechanics of Composites, Texas A&M University, 1989.

Center, Langley Research, ed. Micromechanics analysis of space simulated thermal deformations and stresses in continuous fiber reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Patrick, Dunn, and United States. National Aeronautics and Space Administration., eds. An evaluation of a coupled microstructural approach for the analysis of functionally graded composites via the finite-element method. [Washington, DC: National Aeronautics and Space Administration, 1995.

Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

C, Smith, Lumban-Tobing F, and Langley Research Center, eds. Analysis of thick sandwich shells with embedded ceramic tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

United States. National Aeronautics and Space Administration., ed. An evaluation of the Iosipescu specimen for composite materials shear property measurement. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1991.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

S, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Geometrical modelling of textile reinforcements: Final technical report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Rubin, Devon I., and Jasper R. Daube. Clinical Neurophysiology. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780190259631.001.0001.

MARROQUÍN-DE JESÚS, Ángel, Juan Manuel OLIVARES-RAMÍREZ, Andrés DECTOR-ESPINOZA, and Luis Eduardo CRUZ-CARPIO. CIERMMI Women in Science Biology, Chemistry and Life Sciences Handbook T-XIV. ECORFAN-Mexico, S.C., 2021. http://dx.doi.org/10.35429/h.2021.14.1.119.

Krasnopolskaia, Iuliia. Design and Parametric Modeling of Pretensioned and Stiffened Membranes Project Work. Technische Universität Dresden, 2021. http://dx.doi.org/10.25368/2022.407.