Finite Element Prediction of Structural Failure of Space Payloads under Random Excitation using Different Solvers
Journal: International Journal of Analytical, Experimental and Finite Element Analysis (Vol.3, No. 3)Publication Date: 2017-01-01
Authors : Nirav Modi Hemant Arora Rupali Sahu;
Page : 41-45
Keywords : Random Vibration; Dynamic Simulation; Spacecraft payload;
Abstract
Space payloads are analyzed for their natural frequencies, and for survival under inertial loads and random excitation. In this paper, response of a typical space payload under Random Vibration is studied using Hypermesh/Optistruct and Nastran/Patran. Quadrilateral and Hexagonal elements used in the mesh to obtain higher accuracy and conservative results. Gaussian distribution with Kurtosis control 7 is used predict possible failure of the payload. Comparison of the results obtained by two solvers is made. A possible explanation to the difference in the results is also presented. The explanation helps to approximate results closer to theoretical values and the Gaussian distribution of higher order helps to predict failure of space payloads with higher confidence.
Other Latest Articles
- Design and Simulation of Non-linear Adaptive Filters to Forecast Air Pollution
- Experimental, CFD & Parametric Analysis of Super Heater in Bagasse Fired Water Tube Boiler
- Static Structural Analysis of the Crane Hook using Ansys
- Fabrication and Performance Analysis of Water Vortex Power Plant
- Design and Analysis of Torque Handling Capacity of Slot Headed Grub Screw
Last modified: 2019-03-08 02:04:43