Winglets have a significant impact on the aerodynamic performance of aircraft. When aircraft
are in different flight phases such as takeoff, climb, cruise, descent, and landing, traditional …

A passive energy balancing concept for linear actuation is investigated in the current work
by adopting a negative stiffness mechanism. The proposed negative stiffness mechanism …

An aerodynamic analysis is conducted for morphing winglets on a regional aircraft. The
optimum drag, bending moment, stall angle and maximum lift coeffcient are evaluated for …

Morphing structures suitable for unmanned aerial vehicles (UAVs) have been investigated
for several years. This paper presents a novel lightweight, morphing concept based on the …

Presented within this thesis is the preliminary design phases for the development of a
morphing winglet mechanism. The mathematical models and analyses conducted within this …

This thesis presents a flexible trailing edge mechanism capable of undergoing a change in
camber for a wing section. The mechanism takes advantage of a rigid constraint between …

L'aéronautique actuelle est gouvernée par la transition écologique et le développement
d'avions plus verts. La technologie d'ailes déformables rejoint cette vision nouvelle et a le …

Smart Materials' ability to alter shape by applying an external impetus excitation has
significant potential within the aerospace industry. The ability to operate as an actuator has …

쌍안정성 금속 구조의 파라메트릭 연구 Page 1 한국정밀공학회 2014 년도 춘계학술대회논문집
KSPE 14S422 1. 서론 현대에 이르러 다양한 작업 환경과 요구 조건을 충족시키기 위한 구조체의 …