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  • 1
    facet.materialart.
    Unbekannt
    In:  Other Sources
    Publikationsdatum: 2011-08-16
    Beschreibung: A surface spline is a mathematical tool for interpolating a function of two variables. It is based upon the small deflection equation of an infinite plate. The surface spline depends upon the solution of a system of linear equations, and thus, will ordinarily require the use of a digital computer. The closed form solution involves no functions more complicated than logarithms, and is easily coded. Several modifications which can be incorporated are discussed.
    Schlagwort(e): MATHEMATICS
    Materialart: Journal of Aircraft; 9; Feb. 197
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 2
    Publikationsdatum: 2014-12-18
    Beschreibung: Module design modification requirements for incorporating aeroelastic capabilities into NASTRAN structural analysis program
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA. Langley Res. Center NASTRAN: Users Experiences; p 779-795
    Format: text
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  • 3
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2016-06-07
    Beschreibung: An overview of four analysis capabilities, which developed and integrated into the NASTRAN Thermal Analyzer, is given. To broaden the scope of applications, these additions provide the NTA users with the following capabilities: (1) simulating a thermal louver as a means of the passive thermal control, (2) simulating a fluid loop for transporting energy as a means of the active thermal control, (3) condensing a large sized finite element model for an efficient transient thermal analysis, and (4) entering multiple boundary condition sets in a single submission for execution in steady state thermal analyses.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASTRAN: User's Experiences; p 119-126
    Format: application/pdf
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  • 4
    facet.materialart.
    Unbekannt
    In:  CASI
    Publikationsdatum: 2016-06-07
    Beschreibung: A development for NASTRAN which facilitates the analysis of structures made up of identical segments symmetrically arranged with respect to an axis is described. The key operation in the method is the transformation of the degrees of freedom for the structure into uncoupled symmetrical components, thereby greatly reducing the number of equations which are solved simultaneously. A further reduction occurs if each segment has a plane of reflective symmetry. The only required assumption is that the problem be linear. The capability, as developed, will be available in level 16 of NASTRAN for static stress analysis, steady state heat transfer analysis, and vibration analysis. The paper includes a discussion of the theory, a brief description of the data supplied by the user, and the results obtained for two example problems. The first problem concerns the acoustic modes of a long prismatic cavity imbedded in the propellant grain of a solid rocket motor. The second problem involves the deformations of a large space antenna. The latter example is the first application of the NASTRAN Cyclic Symmetry capability to a really large problem.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASTRAN: Users' Experiences; p 395-421
    Format: application/pdf
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  • 5
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    Unbekannt
    In:  CASI
    Publikationsdatum: 2016-06-07
    Beschreibung: A subsonic flutter analysis capability has been developed for NASTRAN, and a developmental version of the program has been installed on the CDC 6000 series digital computers at the Langley Research Center. The flutter analysis is of the modal type, uses doublet lattice unsteady aerodynamic forces, and solves the flutter equations by using the k-method. Surface and one-dimensional spline functions are used to transform from the aerodynamic degrees of freedom to the structural degrees of freedom. Some preliminary applications of the method to a beamlike wing, a platelike wing, and a platelike wing with a folded tip are compared with existing experimental and analytical results.
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASTRAN: Users' Experiences; p 507-529
    Format: application/pdf
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  • 6
    facet.materialart.
    Unbekannt
    In:  CASI
    Publikationsdatum: 2016-06-07
    Beschreibung: A sample heat transfer analysis is demonstrated which includes the heat of fusion. The method can be used to analyze a system with nonconstant specific heat. The enthalpy is introduced as an independent degree of freedom at each node. The user input consists of a curve of temperature as a function of enthalpy, which may include a constant temperature phase change. The basic NASTRAN heat transfer capability is used to model the effects of latent heat with existing direct matrix output and nonlinear load data cards. Although some user care is required, the numerical stability of the integration is quite good when the given recommendations are followed. The theoretical equations used and the NASTRAN techniques are shown.
    Schlagwort(e): FLUID MECHANICS AND HEAT TRANSFER
    Materialart: NASA. Langley Research Center Computational Aspects of Heat Transfer in Struct.; p 83-89
    Format: application/pdf
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  • 7
    Publikationsdatum: 2019-05-29
    Beschreibung: Axisymmetric Hall current accelerator as electric spacecraft propulsion system
    Schlagwort(e): FACILITIES, RESEARCH, AND SUPPORT
    Materialart: NASA-CR-54705 , EOS-5470-FINAL
    Format: application/pdf
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  • 8
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    In:  Other Sources
    Publikationsdatum: 2019-06-27
    Beschreibung: Ionized plasma electromagnetic accelerators, noting thrust efficiency variation due to difference between supplied and expelled mass flow rate
    Schlagwort(e): PROPULSION SYSTEMS
    Format: text
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  • 9
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    In:  Other Sources
    Publikationsdatum: 2019-06-27
    Beschreibung: Kernel function for nonplanar oscillating surfaces in supersonic flow, using finite element method for interfering configurations
    Schlagwort(e): AERODYNAMICS
    Materialart: ; UG REVUE(
    Format: text
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  • 10
    Publikationsdatum: 2019-06-27
    Beschreibung: Modifications and computational tasks required for aeroelastic capability in NASTRAN
    Schlagwort(e): STRUCTURAL MECHANICS
    Materialart: NASA-CR-111918
    Format: application/pdf
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