Open AccessDesign and Analysis of Double Bobble Cross Section Fuselage Micro-Class Aircraft
Author(s) -
Murlidhar Gupta,
K. Veeranjaneyulu,
MNVS Swetha Bala
Publication year - 2019
Publication title -
international journal of recent technology and engineering
Language(s) - English
Resource type - Journals
ISSN - 2277-3878
DOI - 10.35940/ijrte.d9133.118419
Subject(s) - fuselage , airplane , payload (computing) , lift (data mining) , aerospace engineering , drag , aeronautics , engineering , cross section (physics) , lift to drag ratio , section (typography) , automotive engineering , structural engineering , computer science , physics , computer network , quantum mechanics , network packet , data mining , operating system
The applications of micro-class aircraft is increasing day by day and all industrial community which depending on mobility and surveillance are accepting this type of aircrafts. The main objective of this work is to design and fabricate an aircraft that is capable to carry the highest payload fraction possible with lowest empty weight fraction which all industries required today. Bobble Cross Section Fuselage Micro-Class Aircraft carriers more pay load with maximum lift, minimum airplane weight and drag.