Open AccessEngineering

R. Liebeck

2002.1.14JOURNAL OF AIRCRAFT

DOI: 10.2514/1.9084

Abstract

The Boeing Blended-Wing-Body (BWB) airplane concept represents a potential breakthrough in subsonic transport efficiency. Work began on this concept via a study to demonstrate feasibility and begin development of this new class of airplane. In this initial study, 800-passenger BWB and conventional configuration airplanes were sized and compared for a 7000-n mile design range. Both airplanes were based on engine and structural (composite) technology for a 2010 entry into service

Citation format

LIEBECK, R. Design of the blended wing body subsonic transport. JOURNAL OF AIRCRAFT, 2002, 41: 10–25.