Aerodynamic Efficiency Enhancement of Delta Wings for Micro Air Vehicles Using Shape-Optimization
Author:
Affiliation:
1. Indian Institute of Technology Kharagpur, West Bengal 721 302, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036703
Reference62 articles.
1. Micro- and Nano-Air Vehicles: State of the Art
2. McMichaelJ. M.FrancisM. “Micro Air Vehicles—Toward a New Dimension in Flight,” Defence Advanced Research Projects Agency TTO Document, 1997.
3. Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring
4. The characterization of tandem and corrugated wings
5. Laminar separation bubble characteristics on an airfoil at low Reynolds numbers
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