Includes mechanics and kinematics, used to study the flight stability and control performance of helicopters.

Integrates aesthetics, functionality, and manufacturability to design products that meet user needs.

Uses Computational Fluid Dynamics (CFD) technology to optimize aerodynamic shapes for optimal aerodynamic performance.

Studies the effects of aerodynamic loads on structures during flight to assess the dynamic response and stability of aircraft.

Includes geometric shapes, material selection, and performance calculations to provide the required thrust and efficiency.
Efficiency Calculation: Evaluates propeller performance, including lift, thrust, and power consumption, using theoretical models or experimental tests.

Studies various payloads carried by aircraft, including sensors, cameras, and cargo, to ensure stability and safety during flight.
Structural Strength Calculation: Evaluates the strength and stiffness of aircraft structures based on payload analysis to ensure they can withstand the designed loads.