The purpose of the present work is to analyze the developments of critical technologies for BWB conceptual design from a historical perspective of technology progress. By past decades’ investigations the Blended-Wing-Body (BWB) concept has emerged as a potential solution, which can simultaneously fulfill metrics of noise, emission and fuel burn. The classical Tube-And-Wing (TAW) configuration following the Cayley’s design principles has been optimized to the architecture’s limit, which can hardly satisfy the further requirements on green aviation. Civil aviation faces great challenges because of its robust projected future growth and potential adverse environmental effects.
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