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Journal of the Korea Institute of Military Science and Technology 2007;10(4):73-80.
Flutter Characteristics and Active Vibration Control of Aircraft Wing with External Store
Lae-Hyong Kang, Seung-Jun Lee, In Lee, Jae-Hung Han
KAIST
외부장착물이 있는 항공기 날개의 플러터 특성 및 능동 진동 제어
강래형, 이승준, 이인, 한재흥
한국과학기술원
Abstract
Modern aircraft are required to carry various external stores mounted at different locations on the wing. Sometimes the attachment of stores to an aircraft wing leads to flutter speed reduction, which is a very severe aeroelastic problem. In order to suppress structural vibration and expand the flutter boundary of the aircraft with stores, it is necessary to investigate the main problems and characteristics of them. In addition, active vibration control may be required because passive vibration isolators show limited capabilities for the various wing/store configuration. In this paper, therefore, the flutter stability to the various wing/store configurations was investigated and active vibration control of wing/store model was performed using a piezoelectric actuator.
Key Words: Flutter, Aeroelasticity, Store, Active Control, Vibration Control, Piezoelectric Actuator
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