Aerodynamic Performance of a Hovering Quadcopter Using the Unsteady Vortex Lattice Method
Year: 2025
Type: article
Source: Journal of Aircraft
DOI: 10.2514/1.c038145
Institutions: University of New Mexico, Universidad de Los Andes
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4407259061
