Design and performance analysis of a high-subsonic middle range jetliner: A conceptual approach

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.