Quasi-3D Aerodynamic Analysis Method for Blended-Wing-Body UAV Configurations

Quasi-3D Aerodynamic Analysis Method for Blended-Wing-Body UAV Configurations

The current study presents a low-fidelity, quasi-3D aerodynamic analysis method for Blended-Wing-Body (BWB) Unmanned Aerial Vehicle (UAV) configurations. A tactical BWB UAV experimental prototype is used as a reference platform. The method utilizes 2D panel method analyses and theoretical aerodynami...

Full description

Bibliographic Details
Main Authors: Pericles Panagiotou, Thomas Dimopoulos, Stylianos Dimitriou, Kyros Yakinthos
Format: Article
Language:English
Published: MDPI AG 2021-01-01
Series:Aerospace
Subjects:
UAV
BWB
low-fidelity
aerodynamic analysis
CFD
Online Access:https://www.mdpi.com/2226-4310/8/1/13

Internet

https://www.mdpi.com/2226-4310/8/1/13

Similar Items