2016
DOI: 10.1016/j.prostr.2016.06.411
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Development of Fatigue Loading Spectra from Flight Test Data

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Cited by 7 publications
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“…For the engine's three working states (ground idling, cruising, and maximum- Table 1: 1000 h load spectrum of an aero-engine [25]. The static frequency is only related to the material properties and geometric structure of the turbine blade.…”
Section: Static Finite Element Analysismentioning
confidence: 99%
“…For the engine's three working states (ground idling, cruising, and maximum- Table 1: 1000 h load spectrum of an aero-engine [25]. The static frequency is only related to the material properties and geometric structure of the turbine blade.…”
Section: Static Finite Element Analysismentioning
confidence: 99%