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Cited article:

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A Review on Aero-Engine Inlet-Compressor Integration and Inlet Flow Distortion in Axial Compressors

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Wind tunnel investigation of different engine layouts of a blended-wing-body transport

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Assessment on critical technologies for conceptual design of blended-wing-body civil aircraft

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Chinese Journal of Aeronautics (2019)
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Effects of stability margin and thrust specific fuel consumption constrains on multi-disciplinary optimization for blended-wing-body design

Minghui ZHANG, Zhenli CHEN, Zhaoguang TAN, Wenting GU, Dong LI, Changsheng YUAN and Binqian ZHANG
Chinese Journal of Aeronautics 32 (8) 1847 (2019)
https://doi.org/10.1016/j.cja.2019.05.018