Design Optimization of Aircraft Engine Mount Systems

Design optimization of aircraft engine-mount systems for vibration isolation is presented. The engine is modeled as a rigid body connected to a flexible base representing the nacelle. The base (nacelle) is modeled with mass and stiffness matrices and structural damping using finite element modeling....

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Journal Title: Journal of Vibration and Acoustics Vol. 115; no. 4; pp. 463 - 467
Author: Hashem Ashrafiuon
Format: Article
Published: Oct 1993
Subjects:
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