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  • 1
    Publication Date: 2006-06-26
    Description: Progress in the development of verified design technology for generic advanced-composite structural components loaded in compression is reported. Generic structural configurations material systems and load ranges of interest for a given application were investigated using structural procedures, structural analysis procedures, and laboratory testing of structural specimens. Both flat and curved composite compression panels that are designed either to be buckling resistant or to have postbuckling strength depending on the expected application of the panels were considered.
    Keywords: COMPOSITE MATERIALS
    Type: Selected NASA Res. in Composite Mater. and Struct.; p 35-78
    Format: text
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  • 2
    Publication Date: 2011-08-18
    Description: The ultrasonic group velocity and attenuation were measured as a function of frequency for longitudinal and shear waves in the Hercules epoxy matrix (3501-6) and in the principal directions of the unidirectional Hercules graphite fiber epoxy composite (AS/3501-6). Tests were conducted in the frequency ranges 0.25-14 MHz and 0.5-3 MHz for longitudinal and shear wave modes, respectively. While the attenuation increased with frequency for all wave modes, the group velocity was independent of frequency for all wave modes. In studying the effects of transducer-specimen interface couplant and pressure, it was found that for each transducer, there exists a frequency-dependent 'saturation pressure' corresponding to the maximum output amplitude of the signal.
    Keywords: COMPOSITE MATERIALS
    Type: Journal of Nondestructive Evaluation; 1; June 198
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: An improved procedure for the three dimensional finite element analysis of an angle ply laminate with a circular hole is discussed. The procecure exploits polar symmetry and is the basis for a new finite element computer code. For the broad class of laminates that contain angle plies, this code requires only one half as much computing capacity as conventional codes.
    Keywords: COMPOSITE MATERIALS
    Type: NASA-TM-81852
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-27
    Keywords: COMPOSITE MATERIALS
    Type: NASA-CR-159345 , AD-B046801
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-13
    Description: Angleplied laminates of high modulus graphite fiber/epoxy were examined in several ply configurations at various tensile loading angles to the zero ply direction to determine the effects of ply orientations on tensile properties, fracture modes, and fracture surface characteristics of the various plies. Experimental results consist of stress-strain data, selected plots, fracture stresses and strains, and scanning electron microscope (SEM) photographs of fracture surfaces. It was found that the stress-strain curves were linear to fracture, and that although fracture surface characteristics for a given fracture mode are similar to those for the same fracture mode in uniaxial specimens, no simple load angle range can be associated with a given fracture mode. It was also concluded that SEM results must be supplemented with ply stress calculations in order to identify ranges of fracture modes occurring as a function of ply orientation with respect to the load direction.
    Keywords: COMPOSITE MATERIALS
    Type: Rising to the challenge of the ''80s; Annual Conference and Exhibit; Feb 04, 1980 - Feb 08, 1980; New Orleans, LA
    Format: text
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  • 6
    Publication Date: 2019-07-13
    Description: Angelplied laminates of high modulus graphite fiber/epoxy were studied in several ply configurations at various tensile loading angles to the zero ply direction in order to determine the effects of ply orientations on tensile properties, fracture modes, and fracture surface characteristics of the various plies. It was found that fracture modes in the plies of angleplied laminates can be characterized by scanning electron microscope observation. The characteristics for a given fracture mode are similar to those for the same fracture mode in unidirectional specimens. However, no simple load angle range can be associated with a given fracture mode.
    Keywords: COMPOSITE MATERIALS
    Type: NASA-TM-81405 , E-319 , Ann. Conf. of the Reinforced Plastics/Composites Inst.; Feb 04, 1980 - Feb 08, 1980; New Orleans
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