A new reverse educing method (REM) is presented to estimate the vibrational stress on rotating aeroengine blades from the actual fracture section. This method does not conform to the traditional calculating method, but involves the reverse solution idea. The value of the crack propagation ratio da/dN can be obtained from the actual fracture section of the blade, and then the vibrational stress on rotating blades can be calculated through static computation, modal analysis and crack stress intensity factor calculation. The result is very significant for fault diagnosing and shooting of aeroengine blades.
A new method to calculate the vibrational stress of rotating blades
Aircraft Engineering and Aerospace Technology ; 73 , 1 ; 26-30
2001-02-01
5 pages
Article (Journal)
Electronic Resource
English
A new method to calculate the vibrational stress of rotating blades
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