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Quantitative Comparison of 2D and 3D Shock Control Bumps for Drag Reduction on Transonic Wings
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
- United Kingdom
doi 10.1177/0954410018778815
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Categories
Mechanical Engineering
Aerospace Engineering
Date
May 29, 2018
Authors
Feng Deng
Ning Qin
Publisher
SAGE Publications
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