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- W2356005513 abstract "It is taken the first which helicopter tail rotor dynamic sign is analysed,the reson for failure was analysed from affecting dynamic characteristic side,the reson for failure has been confirmed when it combined with fault tail rotor checking in further.At last the procedure of analyzing failure reason has been provided." @default.
- W2356005513 created "2016-06-24" @default.
- W2356005513 creator A5051031996 @default.
- W2356005513 date "2009-01-01" @default.
- W2356005513 modified "2023-09-23" @default.
- W2356005513 title "Application of Dynamic Analysis In Helicopter Tail Rotor Failure Analysis" @default.
- W2356005513 hasPublicationYear "2009" @default.
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