Minimum Induced Drag for Tapered Wings Including Structural Constraints
Author:
Affiliation:
1. Utah State University, Logan, Utah 84322-4130
Funder
Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035757
Reference34 articles.
1. PrandtlL. “Applications of Modern Hydrodynamics to Aeronautics,” NACA TR-116, June 1921.
2. Lifting-Line Analysis for Twisted Wings and Washout-Optimized Wings
3. Minimizing Induced Drag with Wing Twist, Computational-Fluid-Dynamics Validation
4. Preliminary-Design Aerodynamic Model for Complex Configurations Using Lifting-Line Coupling Algorithm
5. Lifting-Line Predictions for Induced Drag and Lift in Ground Effect
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