Abstract. This study describes the establishment of similarity conditions among structural systems. The main objective of this research is to study the applicability of similitude theory in establishing necessary similarity ...

This paper presents the similarity conditions between aeroelastic instability (flutter) and the free vibration frequency of cross-ply laminated plate. The method is based upon the direct use of governing equation of the ...

در این مقاله اثر لایه پیزوالکتریک به عنوان یک خود-حسگر و خود-محرک بر روی پاسخ یک صفحه سالم چند لایه متقارن مرکب بصورت تحلیلی مورد بررسی قرار گرفته است. با استفاده از اصل همیلتون معادله حرکت سیستم بدست آمده و مقادیر حاصل ...

Abstract – The performance of segmented piezoelectric actuator in controlling the flutter of a damaged metallic plate is presented in this study. Numerical studies using commercial finite element software were conducted ...

This study describes the establishment of similarity conditions among structural systems. The

main objective of this research is to study the applicability of similitude theory in establishing necessary

similarity ...

The performance of damaged metallic plates reinforced with fiber-reinforced polymer

composite materials (composite patches) is presented in this study. A square aluminum plate with a

central cutout is considered ...

This study investigates the application of laminated composite patches for enhancement

of flutter behavior of perforated metallic plates repaired with an external composite patch.

Due to material anisotropy ...

This study demonstrates the applicability of the similitude theory and scaled models in the prediction of the flutter speed of cross-ply laminated plates subjected to supersonic flow. Such a study is important since it ...

The main objective of this study is to demonstrate the applicability of similitude theory in designing

scaled down models to predict the flutter pressure of delaminated composite beam-plate subjected to

supersonic ...

This study describes the establishment of the necessary similarity conditions for dynamic aeroelastic stability of laminated composite plates. An analytical investigation based on the direct use of the governing equations ...