Title :
Design and performance analysis of a high-subsonic middle range jetliner: A conceptual approach
Author :
M Muhammad;M Arifuzzaman;D Swarnaker;M M N Hossain
Author_Institution :
Department of Aeronautical Engineering, Military Institute of Science and Technology, Dhaka, Bangladesh
Abstract :
This paper represents conceptual design of 450 seated fuel efficient high subsonic middle range passenger aircraft. Here the prime concern is to carry more passengers with reduced ultimate fuel cost. The flight performance analysis is designed to allow pliable variation of cruise, climb and descent segments in the mission profile. Simulation technique is used to find structural analysis and aerodynamic characteristics by numerical transformation of several iteration results.
Keywords :
"Aircraft","Aircraft propulsion","Fuels","Automotive components","Military aircraft","Performance analysis","Atmospheric modeling"
Conference_Titel :
Electrical & Electronic Engineering (ICEEE), 2015 International Conference on
Print_ISBN :
978-1-5090-1939-7
DOI :
10.1109/CEEE.2015.7428246
