Affiliation:
1. Oklahoma State University
Publisher
American Institute of Aeronautics and Astronautics
Reference23 articles.
1. 2Whitcomb, Richard T. “A Design Approach and Selected Wind-Tunnel Results at High Subsonic Speeds for Wing-Tip Mounted Winglets”. NASA TN D-8260, July 1976.
2. DRAG DUE TO LIFT: Concepts for Prediction and Reduction
3. Aerodynamic design and analysis of winglets
Cited by
23 articles.
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