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Showing 1 to 12 of 12 for “"Patran"”.

  1. Finite Element Analysis of Breast Implants

    … work was completed using the commercial codes PATRAN and ABAQUS. PATRAN was used for pre- and post-processing, while ABAQUS was used for the actual analysis and to add fluid and contact elements not supported by PATRAN. Many different loading situations and constraints were applied to these …

    vt Repository record for Finite Element Analysis of Breast Implants (opens in a new tab)

  2. Effect of Fatigue Cycle Loading Amplitude Tension-Tension on Composite Laminated Plates with Initial Delamination

    … with numerical analysis models using Nastran/Patran software .</p> <p>The laminate composite plates were fabricated with woven prepreg carbon fiber with an initial delamination and tested under tensile and constant amplitude cycle loading. The tensile characteristics of the laminated composite …

    calpoly Repository record for Effect of Fatigue Cycle Loading Amplitude Tension-Tension on Composite Laminated Plates with Initial Delamination (opens in a new tab)

  3. Vibration Analysis of a Wind Turbine Multi-Stage Planetary Gearbox Incorporating a Flexible Body Component

    … a multibody dynamic analysis program, and MSC Patran/Nastran, a finite element analysis software, and its associated solver. The model is created to show the vibration patterns of a healthy gearbox with rigid bodies, with a flexible body, and with a defect applied on a particular gear in the …

    calpoly Repository record for Vibration Analysis of a Wind Turbine Multi-Stage Planetary Gearbox Incorporating a Flexible Body Component (opens in a new tab)

  4. Experimental and Computational Analysis of a 3D Printed Wing Structure

    … compared against the commercial software Nastran/Patran. Further plans include experimental aerodynamic test of 3D printed wing in the new Embry-Riddle Aeronautical University’s (ERAU) wind tunnel to validate the proposed model.</p>

    embry-riddle Repository record for Experimental and Computational Analysis of a 3D Printed Wing Structure (opens in a new tab)

  5. Analysis of After Impact Characteristics and Structural Optimization of CFRP Composite Plate

    … Further, the modified model was created in MSC. PATRAN/NASTRAN to optimize the ply thickness, ply orientation, and dimensional properties of the plate to minimize the weight while abiding by the structural response constraints. Moreover, the possibility of the OpenMDAO framework in nonlinear …

    embry-riddle Repository record for Analysis of After Impact Characteristics and Structural Optimization of CFRP Composite Plate (opens in a new tab)

  6. Integrated analyses in plastics forming.

    … section has been modelled and calculated by PATRAN/ABAQUS finite element analysis software and tested. These calculations and analysis are applied to the special case but can be use as an example for general analysis and calculation in the ejection section of plastics forming.

    sheffield-hallam Repository record for Integrated analyses in plastics forming. (opens in a new tab)

  7. Identification and investigation of local optima in aerospace structural design

    … location of an additional rib with the aid of a Patran Command Language (PCL) algorithm. The objective function of minimum weight was approximated as a multimodal function in a 2D smooth curve where the local and global optima were identified. The theory of continuous rectangular plates was used …

    unsw Repository record for Identification and investigation of local optima in aerospace structural design (opens in a new tab)

  8. Design of an active compressor blade for aeroelastic studies

    … properties of the Active Rotor Blade. A NASTRAN/PATRAN finite element model was developed with these design parameters to calculate the stresses in the composite spars, the level of tip rotation available from piezoelectric actuation, and the strains seen by the piezoceramic under full …

    mit Repository record for Design of an active compressor blade for aeroelastic studies (opens in a new tab)

  9. A critical analysis of the acoustic emission technique for NDE of pressure vessels

    … mechanical computer-aided engineering program PATRAN is also used to construct the finite element model and to interpret the stress analysis results. The convenience and the success of these computer programs to handle this kind of problem are confirmed. The application of different types of …

    vt Repository record for A critical analysis of the acoustic emission technique for NDE of pressure vessels (opens in a new tab)

  10. Reliability and failure analysis of composite beams and plates containing stress concentrations

    … dictates. For post-processing purposes, PATRAN and I-DEAS are used. Linear and nonlinear stress analyses were performed for the case of composite plates under transverse loading. A methodology for reliability analysis is developed for composite beams and plates with and without stress …

    vt Repository record for Reliability and failure analysis of composite beams and plates containing stress concentrations (opens in a new tab)

  11. Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures

    … it interacts with the commercial software MSC. Patran (for geometry and mesh creation), MSC. Nastran (for finite element analysis), and MSC. Marc (for damage tolerance analysis). The crack location is set to the location of the maximum value of the major principal stress while its orientation is …

    vt Repository record for Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures (opens in a new tab)

  12. Finite Element Analysis Of A Test Specimen For Strength Of A Co-polymer Layer At A Bone-implant Interface

    The aim of this work is to evaluate the mechanical strength of a co-polymer of 2-hydroxyethylmethacrylate (HEMA) and methylmethacrylate (MMA), so that it can be applied as an interfacial layer between bone cement and steel implants to improve their performance and life. Finite element (FE) analysis …

    ucf