Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV

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Publisher: American Institute of Aeronautics and Astronautics

Publication date (Print): June 05 2006

Publication date (Online): June 15 2006

Publication date (Print): June 05 2006

Publication date (Electronic): June 15 2006

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[1 ]School of Aeronautics, Northwestern Polytechnical University

[2 ]UAV Research and Development Center, Northwestern Polytechnical University

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DOI: 10.2514/6.2006-3462

SO-VID: f40d75d5-3bd7-417c-8c4e-0ef7d30367a2

Conference name: 24th AIAA Applied Aerodynamics Conference

Conference location: San Francisco, California

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Self URI (article page): https://arc.aiaa.org/doi/10.2514/6.2006-3462

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Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV

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