Vibration analysis of an aircraft wing and fuselage made of composite material

The use of composites in ultra-light aircrafts is only natural. Low weight and high strength are two attractive features which make them highly desirable. A newly designed all composite aircraft was to be launched in the market. Stress and Vibration analysis was conducted on the wing and fuselage section of the aircraft, following which it was approved for production. The manufacturer saved on time and physical testing costs.