Invariant Formulation for the Minimum Induced Drag Conditions of Nonplanar Wing Systems
Author:
Affiliation:
1. Department of Aerospace Engineering, San Diego State University, San Diego, California 92182
2. Department of Mathematical Sciences, Politecnico di Torino, 10129 Turin, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052837
Reference48 articles.
1. Experimental Investigation of Wing-Tip Devices on the Reduction of Induced Drag
2. Induced Drag - Historical Perspective
3. DRAG DUE TO LIFT: Concepts for Prediction and Reduction
4. Minimizing Induced Drag with Spanwise Blowing Variation on Circulation-Controlled Wing
5. Minimizing Induced Drag with Wing Twist, Computational-Fluid-Dynamics Validation
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