Lifting-Line Analysis of Wing Twist to Minimize Induced Drag During Pure Rolling Motion
Author:
Affiliation:
1. Utah State University
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2040
Reference77 articles.
1. Variable Camber Compliant Wing - Design
2. Variable Camber Compliant Wing - Wind Tunnel Testing
3. Fluid-Structure Interaction of a Variable Camber Compliant Wing
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