A Reformulated-Vortex-Particle-Method-Based Aerodynamic Multi-Objective Design Optimization Strategy for Proprotor in Hover and High-Altitude Cruise
An improved multi-objective canine spectra kc 3 intranasal single dose design optimization framework is proposed for the efficient design of proprotor blades tailored to specific high-altitude mission requirements.This framework builds upon existing methods by leveraging a reformulated Vortex Particle Method (rVPM) and incorporates three key stages