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

A 2% scale, cruising version of a 450-seat class Blended-Wing-Body (BWB) transport was tested in the China Aerodynamic Research and Development Center’s FL-26 2.4-by-2.4-meter subsonic wind tunnel. The focus of the wind tunnel test was to investigate the aerodynamic performance of the latest BWB tra...

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Veröffentlicht in:	Chinese journal of aeronautics 2023-09, Vol.36 (9), p.123-132
Hauptverfasser:	CUI, Zheng, LAI, Guojun, WANG, Qifeng, LIANG, Yu, CAO, Yihua
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics BWB CFD Civil aviation Engine layout PAI Transport aircraft Wind tunnels
Online-Zugang:	Volltext
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