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Lesson |
Support File |
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Modal Analysis of a Flat Plate: Produce a MSC.Nastran input file and submit for analysis to find the first five natural frequencies and mode shapes. (NAS102) |
N/A |
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Modal Analysis of a Flat Plate Using Static Reduction: Reduce the dynamic math model in the previous exercise to one with fewer degrees of freedom and find the first five natural frequencies. (NAS102) |
N/A |
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Direct Transient Response Analysis: Using the direct method define time-varying excitation and compute nodal displacement for desired time domain. (NAS102) |
N/A |
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Modal Transient Response Analysis: Using the Modal Method define time-varying excitation and compute nodal displacement for desired time domain. (NAS102) |
N/A |
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Direct Frequency Response Analysis: Using the direct method define frequency-varying excitation and compute nodal displacement for desired frequency domain. (NAS102) |
N/A |
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Modal Frequency Response Analysis: Using the Modal Method define frequency-varying excitation and compute nodal displacement for desired frequency domain. (NAS102) |
N/A |
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Direct Transient Response with Base Excitation: Using the direct method define time-varying unit acceleration and compute nodal displacement for desired time domain. (NAS102) |
N/A |
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Enforced Motion with Direct Frequency Response: Using the direct method define frequency-varying tip displacement and compute nodal displacement for desired time domain. (NAS102) |
N/A |
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Response Spectra: Generate a shock spectrum using the direct transient method. (NAS102) |
N/A |
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Response Spectra (Cont.): Apply a shock spectrum. (NAS102) |
N/A |
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Random Analysis: Enforced acceleration using large mass method. (NAS102) |
N/A |
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Random Analysis: Determining the displacement response spectrum from random pressure and force loads with cross spectrum correlation. (NAS102) |
N/A |
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Complex Modes of a Pile Driver: Learn to define complex eigenvalue extraction parameters and compute complex modes. (NAS102) |
N/A |
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Nolins in Linear Transient: Learn to represent non-structural variables using non-structural DOFs, define dynamic functions with transfer functions and create a nonlinear transient force. (NAS102) |
N/A |
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Modal Analysis of a Beam: Perform normal modes analysis and find the first three natural frequencies for a simply supported beam. (NAS102) |
N/A |
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Normal Modes with Differential Stiffness: Analyze a stiffened beam for normal modes. (NAS102) |
N/A |
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Weight Minimization of a Three Bar Truss: Minimize the weight of a truss with mode constraints. (NAS102) |
N/A |
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Modal Analysis of a Beam (SI Units): Analyze a stiffened beam for normal modes. (NAS102) |
N/A |
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Normal Modes with Differential Stiffness (SI Units): Analyze a stiffened beam for normal modes. (NAS102) |
N/A |
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Normal Modes with Differential Stiffness (SI Units): Analyze a stiffened beam for normal modes. (NAS102) |
N/A |