Design and structural analysis off lutter predictionin zodiac CH-601XL aircraft wing to reduce drag

The wings of the aircraft reflect an aircraft's primary lift unit. The aerodynamic strain, weather, wind and vibration are the liability of the aircraft's wing throughout the ride. Aeronautical and structural stresses may often be handled by aircraft wings. Therefore, aircraft wings must be constructed to have good overall efficiency throughout each period of operation, both structurally and aerodynamically. Spar, ribs, thongs and skin are the main structural elements of a wing construction. It is a fluttering experiment regarding the wing and re-designing of zodiac aircraft. The method was identified in the literature survey to decide the current wing design parameters. Here we are exploring the possibility of static aero elastic problems by using PATRAN of FEA softwareMain objective of this project is to makes a stable aircraft wing which can overcome all flutter related problems in the design limit region. We always tried to keep the weight margin in same limit