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  • 1
    Publication Date: 2006-04-02
    Description: Asymptotic solutions of Novozhilov's equations of shells of revolution are derived for axisymmetric and first harmonic loadings. The solutions obtained are valid throughout the shallow and nonshallow regions. Stresses in dome shaped shells of revolution with a discontinuity in the form of a circular hole, a circular rigid insert, or a nozzle at the apex have been investigated. Numerical results are obtained for spheres, ellipsoids, and paraboloids, containing a discontinuity under a internal pressure and moment. Curves depicting stress distributions are given. The influence of three types of discontinuity on the stresses of the shells is also given.
    Keywords: STRUCTURAL MECHANICS
    Type: Multivariant Function Model Generation; 118 p
    Format: text
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  • 2
    Publication Date: 2011-08-18
    Description: The theoretical prediction of the bead area contact load at the tire wheel interface using NASTRAN is reported. The application of the linear code to a basically nonlinear problem results in excessive deformation of the structure and the tire-wheel contact conditions become impossible to achieve. A psuedo-nonlinear approach was adopted in which the moduli of the cord reinforced composite are increased so that the computed key deformations matched that of the experiment. Numerical results presented are discussed.
    Keywords: STRUCTURAL MECHANICS
    Type: Georgia Univ. 10th NASTRAN User's Colloq.; p 133-142
    Format: text
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  • 3
    Publication Date: 2016-06-07
    Description: The derivation is presented of the differential stiffness for triangular solid of revolution elements. The derivation takes into account the element rigid body rotation only, the rotation being about the circumferential axis. Internal pressurization of a pneumatic tire is used to illustrate the application of this feature.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Langley Res. Center NASTRAN: Users' Experiences; p 171-179
    Format: application/pdf
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  • 4
    Publication Date: 2016-06-07
    Description: An application of the membrane element to the problem of the tensioning of a conveyer belt which wraps around a drum is presented. Two cases were investigated: (1) belt tension increase due to drum edge wear; and (2) material trapped between the drum and the belt. In both cases it was found that the increase in belt tension was due to the additional stretching of the belt resulting from the drum radius change rather than from the transverse deflection of the belt.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Goddard Space Flight Center Eighth NASTRAN User's Colloq.; p 33-39
    Format: application/pdf
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  • 5
    Publication Date: 2019-05-29
    Description: Matrix algebra solution, using coordinate systems transformations, to boundary value problem for structures composed of shell elements
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-70187 , M-77-65-7
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  • 6
    Publication Date: 2019-05-29
    Description: Digital programs to determine stiffness influence coefficients of cylindrical, conical, and spherical shell segments by finite difference method
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-70016 , M-77-65-6
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  • 7
    Publication Date: 2019-05-29
    Description: Equations for thin elastic spherical shells and digital program for analysis of stresses and deformation of fixed edge segmental spherical shells - solution by finite difference technique
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-68766 , LMSC-M-77-65-4
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  • 8
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    In:  CASI
    Publication Date: 2019-06-28
    Description: A data base of mechanical and fracture properties for GaAs was generated. The data for single crystal GaAs will be used to design reusable GaAs solar modules. Database information includes; (1) physical property characterizations; (2) fracture behavior evaluations; and (3) strength of cells determined as a function of cell processing and material parameters.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-175657 , JPL-84-81 , NAS 1.26:175657
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  • 9
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    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The fracture mechanics of crystalline Si are reviewed, together with known techniques for minimizing the occurences of fracture and/or their effects. The fracture toughness (Kic) of Si varies only 10 percent from cell-to-cell and standard values have been established for different types of crystalline Si cells. A critical flaw size of 10-100 microns has been identified, and also pertains to polycrystalline materials. Chemical polishing is known to double the value of Kic, while edge rounding has no effect. Internal stresses, particularly those caused during ribbon growth, do not exceed 10 percent of Kic. External stresses are imposed by the module hardware and the ambient environment. Multiple contacts reduce the effects of cell fracture and series-parallel wiring in modules in arrays ameliorates the effects of single-cell failures. During manufacturing, maintenance of quality control and removal of sheets displaying aberrations can, depending on the costs and the implementation of the array reliability features, result in arrays delivering any desired level of reliability.
    Keywords: STRUCTURAL MECHANICS
    Type: Photovoltaic Solar Energy Conference; Oct 17, 1983 - Oct 21, 1983; Athens; Greece
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  • 10
    Publication Date: 2019-07-13
    Description: Fracture of Czochralski silicon wafers during processing is an important factor in solar cell yield and cost. A fracture-mechanics test and analysis program was developed to evaluate fracture strength changes in the in-process wafer-to-cell processing at different stages on a manufacturer's production line. The strength data were described by Weibull statistical analysis and can be interpreted with the surface-flaw distribution of each of the process steps.
    Keywords: STRUCTURAL MECHANICS
    Type: Photovoltaic Specialists Conference; Jan 07, 1980 - Jan 10, 1980; San Diego, CA
    Format: text
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