This study aims to provide the pilot with optimal control time histories for stabilization of a helicopter after releasing the slung load in aerial delivery mis
Tip clearances of multistage rotors and stators greatly affect aero-engines' aerodynamic efficiency, stability and safety. The inevitable machining and assembly
The Unsteady Vortex Lattice Method (UVLM) is a medium-fidelity aerodynamic tool that has been widely used in aeroelasticity and flight dynamics simulations. The