Now a days it is observed that weight parameter is a specific issue for many companies for better efficiency of any
product. So, in recent a specific profile of light weight helicopter blade is designed. Due to composite material of carbon epoxy it
is light in weight but also high strength carrying blade. The main scope of this project is to design a composite rotor blade using
Carbon Fiber and Manufacturing it by using Hand layup process.
In experimentation, Impact hammer test and FFT analyzer will be used for the validation purpose. Natural frequencies for
helicopters blade structure with reinforcement will be calculated. Results and conclusion will be drawn by comparing analytical
and experimental values. Suitable material will be suggested by analyzing the data along with future scope.
