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Indian Institute of Engineering Science and Technology, Department of Aerospace Engineering and Applied Mechanics, India
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Drag Reduction and Turbulent Characteristics of a Low Aspect Ratio Wing with Fluidic On-Demand Winglet

SAE International Journal of Aerospace

  • Journal Article
  • 01-16-01-0003
Published 2022-04-20 by SAE International in United States
Annotation ability available