Modeling and Vibration Suppression of Flexible Spacecraft Using Higher-Order Sandwich Panel Theory

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چکیده

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ژورنال

عنوان ژورنال: The International Journal of Acoustics and Vibration

سال: 2017

ISSN: 1027-5851,2415-1408

DOI: 10.20855/ijav.2017.22.2459