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  • Other Sources  (88)
  • STRUCTURAL MECHANICS  (88)
  • 1985-1989  (47)
  • 1965-1969  (38)
  • 1960-1964  (3)
  • 1
    Publication Date: 2013-08-31
    Description: A global/local time incrementing scheme for viscoplastic analysis of structures is presented. The scheme is very efficient and useful for conducting large scale nonlinear finite element analysis involving viscoplastic materials.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Lewis Research Center, Nonlinear Constitutive Relations for High Temperature Applications, 1986; p 307-315
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  • 2
    Publication Date: 2006-10-26
    Description: Structural dynamics, and results of finite element modelling of thin plates
    Keywords: STRUCTURAL MECHANICS
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  • 3
    Publication Date: 2006-10-26
    Description: Elastic instability of pressurized cylindrical shells under compression or bending
    Keywords: STRUCTURAL MECHANICS
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  • 4
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    In:  Other Sources
    Publication Date: 2011-08-11
    Description: Small amplitude vibrations of rectangular panel relative to static buckled configuration
    Keywords: STRUCTURAL MECHANICS
    Type: AMERICAN SOCIETY OF CIVIL ENGINEERS
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  • 5
    Publication Date: 2013-08-31
    Description: The demand on safety performance of launching structure and equipment system from impulsive excitations necessitates a study which predicts the maximum response of the system as well as the maximum stresses in the system. A method to extract higher modes and frequencies for a class of multiple degree-of-freedom (MDOF) Structure system is proposed. And, along with the shock spectra derived from a linear oscillator model, a procedure to obtain upper bound solutions for maximum displacement and maximum stresses in the MDOF system is presented.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA, John F. Kennedy Space Center, NASA(ASEE Summer Faculty Fellowship Program: 1988 Research Reports; p 42-77
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  • 6
    Publication Date: 2013-08-31
    Description: A major research and technology program in Probabilistic Structural Analysis Methods (PSAM) is currently being sponsored by the NASA Lewis Research Center with Southwest Research Institute as the prime contractor. This program is motivated by the need to accurately predict structural response in an environment where the loadings, the material properties, and even the structure may be considered random. The heart of PSAM is a software package which combines advanced structural analysis codes with a fast probability integration (FPI) algorithm for the efficient calculation of stochastic structural response. The basic idea of PAAM is simple: make an approximate calculation of system response, including calculation of the associated probabilities, with minimal computation time and cost, based on a simplified representation of the geometry, loads, and material. The deterministic solution resulting should give a reasonable and realistic description of performance-limiting system responses, although some error will be inevitable. If the simple model has correctly captured the basic mechanics of the system, however, including the proper functional dependence of stress, frequency, etc. on design parameters, then the response sensitivities calculated may be of significantly higher accuracy.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Lewis Research Center, Structural Integrity and Durability of Reusable Space Propulsion Systems; p 145-151
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  • 7
    Publication Date: 2016-06-07
    Description: Due to the stringent design requirement for aerospace or nuclear structural components, considerable research interests have been generated on the development of constitutive models for representing the inelastic behavior of metals at elevated temperatures. In particular, a class of unified theories (or viscoplastic constitutive models) have been proposed to simulate material responses such as cyclic plasticity, rate sensitivity, creep deformations, strain hardening or softening, etc. This approach differs from the conventional creep and plasticity theory in that both the creep and plastic deformations are treated as unified time-dependent quantities. Although most of viscoplastic models give better material behavior representation, the associated constitutive differential equations have stiff regimes which present numerical difficulties in time-dependent analysis. In this connection, appropriate solution algorithm must be developed for viscoplastic analysis via finite element method.
    Keywords: STRUCTURAL MECHANICS
    Type: Nonlinear Constitutive Relations for High Temp. Appl., 1984; p 187-200
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  • 8
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    In:  CASI
    Publication Date: 2016-06-07
    Description: Multiaxial testing methods are reviewed. Advantages and disadvantages of each type test is discussed. Significant multiaxial data available in the literature is analyzed. The yield theories are compared for multiaxial fatigue analysis.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Lewis Research Center Nonlinear Constitutive Relations for High Temp. Appl., 1984; p 221-236
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  • 9
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    In:  CASI
    Publication Date: 2013-08-31
    Description: The functional, structural adequacy of a 20 meter long generic space truss (Mini-Mast), subjected to fatigue loading, was examined with respect to the failure modes which are most likely to occur during services. The space truss is made of thin-walled tubes having unidirectional, zero degree layups of Celanese G50 graphite fibers/Narmco 5217 epoxy composites. The approach used to investigate the most probable failure mode of the truss under fatigue loading is to determine the stress level, including the types of stress, in the member first, then followed by failure mode analysis based on the stress level just determined. To begin, an approximate beam-parameter truss (BPT) model is analyzed first, followed by a detailed analysis of the truss using a finite element model (FEM) run with NASTRAN code. The response results of the BPT model are used to compare FEM results and to check any major deviation of trend derived from the FEM. The purpose of the work was to search available fatigue data of the tube material, to conduct approximate dynamical stress analysis of the BPT model, to run detailed dynamical stress analysis of the FEM model using NASTRAN code, and to predict the fatigue life of the truss member based on limited fatigue data.
    Keywords: STRUCTURAL MECHANICS
    Type: Old Dominion Univ., NASA/American Society for Engineering Educ; Old Dominion Univ.,
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  • 10
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    In:  Other Sources
    Publication Date: 2011-08-19
    Keywords: STRUCTURAL MECHANICS
    Type: Finite Elements in Analysis and Design (ISSN 0168-874X); 5; 269-279
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