Regina V. Leonteva, Mikhail A. Pronin, Vsevolod I. Smyslov

DOI Number: N/A

Conference number: IFASD-2017-114

Theoretical basics and the analysis of ground simulations’ features of airplane forced vibrations after engine blade off, technical means and the experimental procedure are given. Examples of simulation predictions of airplane vibrations with the engine imbalance obtained during standard ground vibration tests (GVT) are given.

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In Categories: 1. IFASD 2017, 1.Events, Dynamic loads
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