Wing Design for Class I Mini Unmanned Aerial Vehicles—Special Considerations for Foldable Wing Configuration at Low Reynolds Numbers

Wing Design for Class I Mini Unmanned Aerial Vehicles—Special Considerations for Foldable Wing Configuration at Low Reynolds Numbers

Foldable wing designs are becoming increasingly popular due to their advantages in the rapid deployment and compact packaging of fixed-wing UAVs, particularly when compared to horizontal take-off and VTOL counterparts. However, selecting an appropriate wing design requires the careful consideration...

Full description

Saved in:
Bibliographic Details
Main Authors: Eleftherios Karatzas, Eleftherios Nikolaou, Antonis Pitsis, Spiridon Alexopoulos, Vaios Lappas, Vassilis Kostopoulos
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Engineering Proceedings
Subjects:
wing design
foldable wing
conceptual design
Online Access:https://www.mdpi.com/2673-4591/90/1/96
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items

Similar Items