- Shock and vibration analysis can be performed either in the frequency or time domain
- The time domain method requires more computation time but is much better suited for transient and nonstationary excitation
- Time domain methods are also better for rainflow fatigue cycle counting
- Students should already have some familiarity with Femap & Nastran
- They should also be able to perform SRS time history synthesis as shown in previous Vibrationdata units
- NX Nastran is used as the solver, but the methods should work with other versions
- Two units for direct shock response spectrum analysis is also included
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Prerequisite Materials
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Main Presentations:
Nastran Modal Transient Slides: 200_FEA_modal_transient_revJ.pptx & Alternate Link
Nastran FEA Base Excitation via Response Spectrum: 201_FEA_response_spectrum_revE.pptx & Alternate Link
Nastran FEA Base Excitation with Multiple Response Spectrum Inputs: 202_FEA_response_spectrum_multiple_revA.pptx & Alternate Link
Nastran FEA Frequency Response Function for Base Input:
203_FEA_frf_revB.pptx & Alternate Link
FEA PSD Response for Base Excitation using Femap, Nastran & Matlab: 204_FEA_psd.pptx & Alternate Link
Avionics Component Shock Sensitivity & FEA Shock Analysis: avionics_box_fea_shock.pptx & Alternate Link
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Nastran Files
Students should generate their own files, but here are several for reference:
square_plate_modal_transient_seismic_mass.bdf
square_plate_response_spectrum.bdf
square_plate_response_spectrum_multiple.bdf
Nastran Acceleration Time History: srs2000G_accel.nas
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See also: Vibrationdata Nastran
– Tom Irvine
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