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TutorialsEquivalent Static Load for Random Vibration. The static load is taken from the three-sigma vibration response: eqstatic.pdfRelated Rayleigh distribution program: peak_response_random.exe |
H.M. Lee, Testing for Random Limit Load Versus Static Limit Load, NASA TM-108542: Lee1.pdfH.M. Lee, A Simplistic Look at Limit Stresses from Random Loading, NASA TM-108427: Lee2.pdfForce-limited Acceleration Spectra Derivation by Random Vibration Analysis: Methodological Cases and Industrial Application: Trittoni_Force_limited.pdfIntroduction to the Vibration Response Spectrum: vrs.pdfDerivation of Miles Equation for Base Excitation: Miles.pdfSee also: Vibration Response Spectrum |
Cantilever Beam AnalysisEquivalent Static Load for a Cantilever Beam Subjected to Base Excitation, Part I: Sine Input: eqs_cantilever.pdfSteady-State Vibration Response of a Cantilever Beam Subjected to Base Excitation: steady_cant.pdf
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Robert L. Towner, NASAPractical Approach for Random Load Factors RLF.pdfPowerPoint Presentation, FEA model, and Hand-calculation notes RandomLoadFactors.pdf |
software_alt Description |
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Vibration response spectrum of a single-degree-of-freedom system subjected to base excitation. |
vrs.exe |
vrs.cpp |
SDOF fatigue calculation for a given PSD input. The fatigue metric is in terms of acceleration raised to a fatigue exponent. |
vrs_fatigue.exe |
vrs_fatigue.cpp |
SDOF fatigue calculation for a given base excitation time history. The fatigue metric is in terms of acceleration raised to a fatigue exponent. |
qsrs_fatigue.exe |
qsrs_fatigue.cpp |
Response of an individual single-degree-of-freedom system to base excitation. |
sdof_ran.exe |
sdof_ran.cpp |
Response of an individual single-degree-of-freedom system to base excitation via Miles equation. |
miles.exe |
miles.cpp |