Finite Element & CFD based-Design Optimization is a key aspect in the development of Vertical Take-Off and Landing (VTOL), Electric Vertical Take-Off and Landing (e-VTOL), and Urban Air Mobility (UAM) vehicles. These vehicles are rapidly gaining popularity in the Aerospace and Defense industry due to their ability to operate in urban environments, reduce travel time and improve mobility.
Design optimization using FEA and CFD simulations allows engineers to evaluate the aerodynamic performance, structural integrity, and overall efficiency of VTOL, e-VTOL, and UAM vehicles. FEA simulations are used to evaluate the structural integrity of the vehicle's components under various loads, such as centrifugal forces, Crash test and Crashworthiness, thermal stresses, and vibration. CFD simulations are used to evaluate the aerodynamic performance of the vehicle, including drag and lift forces, air flow patterns, and the effects of turbulence.
Additionally, FEA & CFD-based optimization allows for the evaluation of various design parameters such as wing shape, rotor design, motor placement, and battery placement, to determine the optimal configuration for the vehicle. This can lead to improved performance, increased range, and reduced noise levels and optimized acoustics performance.
