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  • 1
    Publication Date: 2006-10-26
    Description: Resonant vibration of a liquid filled circular cylindrical shell
    Keywords: STRUCTURAL MECHANICS
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  • 2
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    In:  CASI
    Publication Date: 2016-06-07
    Description: A state-of-the-art review of applicable constitutive models with selection of two for detailed comparison with a wide range of experimental tests was conducted. The experimental matrix contained uniaxial and biaxial tensile, creep, stress relaxation, and cyclic fatigue tests at temperatures to 1093 C and strain rates from .0000001 to .001/sec. Some nonisothermal cycles will also be run. The constitutive models will be incorporated into the MARC finite element structural analysis program with a demonstration computation made for advanced turbine blade configuration. In the code development work, particular emphasis is being placed on developing efficient integration algorithms for the highly nonlinear and stiff constitutive equations. Another area of emphasis is the appropriate and efficient methodology for determing constitutive constants from a minimum extent of experimental data.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984; 8 p
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  • 3
    Publication Date: 2013-08-31
    Description: The fourth and final year of the HOST project with the initial objective of developing a unified constitutive model for finite element structural analysis of turbine engine hot section components is discussed. The final year's work was primarily concerned with the study of nonisothermal problems and the potential for thermal history effects to occur explicitly in the constitutive equations.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987; p 273-279
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  • 4
    Publication Date: 2019-05-30
    Description: Liquid instability of vibrating partially filled elastic tank, emphasizing resonant breathing mode and frequency response
    Keywords: STRUCTURAL MECHANICS
    Type: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
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  • 5
    Publication Date: 2019-05-29
    Description: Resonant frequencies and mode shapes of truncated conical shells with free edges in transverse vibration
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-384
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  • 6
    Publication Date: 2019-05-24
    Description: Resonant frequencies and mode shapes for transverse vibration of truncated conical shells obtained by considering effect of bending, membrane rigidity and inertia terms due to transverse motion
    Keywords: STRUCTURAL MECHANICS
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  • 7
    Publication Date: 2019-05-30
    Description: Resonant frequencies and associated mode shapes of transverse vibrations of truncated conical shells over wide range of geometrical and modal parameters
    Keywords: STRUCTURAL MECHANICS
    Type: INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES
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  • 8
    Publication Date: 2019-05-23
    Description: Resonant frequencies and associated mode shapes of truncated conical shells over wide range of geometrical and modal parameters
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-62573
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  • 9
    Publication Date: 2019-06-28
    Description: Unified constitutive models are characterized by the use of a single inelastic strain rate term for treating all aspects of inelastic deformation, including plasticity, creep, and stress relaxation under monotonic or cyclic loading. The structure of this class of constitutive theory pertinent for high temperature structural applications is first outlined and discussed. The effectiveness of the unified approach for representing high temperature deformation of Ni-base alloys is then evaluated by extensive comparison of experimental data and predictions of the Bodner-Partom and the Walker models. The use of the unified approach for hot section structural component analyses is demonstrated by applying the Walker model in finite element analyses of a benchmark notch problem and a turbine blade problem.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Lewis Research Center, Nonlinear Constitutive Relations for High Temperature Applications, 1986; p 371-394
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  • 10
    Publication Date: 2019-06-28
    Description: This report presents the results of the second year of work on a problem which is part of the NASA HOST Program. Its goals are: (1) to develop and validate unified constitutive models for isotropic materials, and (2) to demonstrate their usefulness for structural analyses of hot section components of gas turbine engines. The unified models selected for development and evaluation are that of Bodner-Partom and Walker. For model evaluation purposes, a large constitutive data base is generated for a B1900 + Hf alloy by performing uniaxial tensile, creep, cyclic, stress relation, and thermomechanical fatigue (TMF) tests as well as biaxial (tension/torsion) tests under proportional and nonproportional loading over a wide range of strain rates and temperatures. Systematic approaches for evaluating material constants from a small subset of the data base are developed. Correlations of the uniaxial and biaxial tests data with the theories of Bodner-Partom and Walker are performed to establish the accuracy, range of applicability, and integability of the models. Both models are implemented in the MARC finite element computer code and used for TMF analyses. Benchmark notch round experiments are conducted and the results compared with finite-element analyses using the MARC code and the Walker model.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-174980 , NAS 1.26:174980 , SWRI-7576/30 , ASR-2
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