Minimizing Induced Drag with Wing Twist, Computational-Fluid-Dynamics Validation
Author:
Affiliation:
1. Utah State University, Logan, Utah 84322-4130
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.15089
Reference19 articles.
1. Lifting-Line Analysis for Twisted Wings and Washout-Optimized Wings
2. Lifting-Line Analysis of Roll Control and Variable Twist
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