Passive shock wave/boundary layer control of wing at transonic speeds

Passive shock wave/boundary layer control of wing at transonic speeds

At supercritical conditions a porous strip (or slot strip) placed beneath a shock wave can reduce the drag by a weaker lambda shock system, and increase the buffet boundary, even may increase the lift. Passive shock wave/boundary layer control (PSBC) for drag reduction was conducted by SC(2)-0714 su...

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Bibliographic Details
Main Authors: Ling Zhou, Dehua Chen, Yang Tao, Guangyuan Liu, Shuheng Song, Shidong Zhong
Format: Article
Language:English
Published: Elsevier 2017-11-01
Series:Theoretical and Applied Mechanics Letters
Subjects:
Wing
Shock wave/boundary layer interaction
Bump
Drag reduction
Transonic
Optimization design
Online Access:http://www.sciencedirect.com/science/article/pii/S2095034917301319

Internet

http://www.sciencedirect.com/science/article/pii/S2095034917301319

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