Open AccessFlying Wing
Author(s) -
Dávid Pastír,
Miroslava Čičváková
Publication year - 2020
Publication title -
acta avionica
Language(s) - English
Resource type - Journals
eISSN - 1339-9853
pISSN - 1335-9479
DOI - 10.35116/aa.2020.0013
Subject(s) - fuselage , wing , payload (computing) , aeronautics , aerospace engineering , engineering , wing loading , range (aeronautics) , computer science , aerodynamics , angle of attack , computer security , network packet
The aim of the article is to analyse the functionality of Flying Wing design by TU delft and KLM. Flying wing design is a design mainly used in military. This design was used for a strategic bomber which needed to have a long specific range while carrying a heavy payload. This design consists of a single wing which serves as well as a fuselage. This wing fuselage needs to meet airlines requirements.