Conceptual Aerodynamic Studies Of A Small Tailless Unmanned Air Vehicle

In principle, the tailless model configuration can be equipped with any airfoil as long as the design is compensated with an appropriate combination of some parameter such as aspect ratio, sweep angle and twist. This thesis presents a parametric study of subsonic Tailless UAV conceptual design with...

Full description

Saved in:
Bibliographic Details
Main Author: Hashim, Afida
Format: Thesis
Published: 2014
Online Access:
Tags: Add Tag
No Tags, Be the first to tag this record!