Blended Wing Body Thrust Reverser Cascade Feasibility Evaluation Through CFD

Blended Wing Body Thrust Reverser Cascade Feasibility Evaluation Through CFD

Airplane thrust reverser could significantly reduce the landing distance of a conventional civil turbofan. Control of the thrust reverser can be performed by a hydraulic and/or electric system. This study investigates whether this system can be used for blended wing body (BWB) civil airplanes as the...

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Bibliographic Details
Main Authors: Yu Gang, Li Dong, Chen Zhenli, Zhang Zeyu
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Blended wing body
cascade thrust reverser
CFD
landing configuration
Online Access:https://ieeexplore.ieee.org/document/8880660/

Internet

https://ieeexplore.ieee.org/document/8880660/

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