Calculation of vibration modes and resonance frequencies of the Northrop NF-5

Report (1975)

Authors

H.H. Ottens

Finite element method Dynamic analysis Aircraft structure Component mode technique

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Published Date

15-04-1975

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Abstract

The component mode technique is used to calculate resonance frequencies and vibration modes of the Northrop NF-5 structure. The results of the calculations are compared with those of a ground vibration test.

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