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Optimization design study of low-Reynolds-number high-lift airfoils for the high-efficiency propeller of low-dynamic vehicles in stratosphere

  • Published:2010-09-02 Issue:10 Volume:53 Page:2792-2807
  • ISSN:1674-7321
  • Container-title:Science China Technological Sciences
  • language:en
  • Short-container-title:Sci. China Technol. Sci.

Author:

Ma Rong,Zhong BoWen,Liu PeiQing

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference22 articles.

1. Lewis J, Geoffrey S S, Isaac R. Porche III. High-altitude airships for the future force army. Technical Report (TR-234), 2005

2. Hao P F. The Future Stratospheric Airships. Beijing: Chinese Newlore Magazine, 2006. 12

3. Marcus Y, Stephanie K. An overview of advanced concepts for near-space systems. AIAA-2009-4805, 2009

4. Anthony C, Geoffrey A L. Long duration solar flight on venus. AIAA-2005-7156, 2005

5. Mueller T J. The influence of laminar separation and transition on low Reynolds number airfoil hysteresis. J Aircraft, 1985, 22: 764–770

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2. High-altitude airship variable-pitch propeller performance analysis at multiple altitudes;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-04-13

3. High-fidelity multi-level efficiency optimization of propeller for high altitude long endurance UAV;Aerospace Science and Technology;2023-02

4. Optimization Design of Propeller for Ultra-high-altitude Unmanned Aerial Vehicle;Journal of Physics: Conference Series;2022-11-01

5. Aerodynamic optimization of a propeller airfoil at low Reynolds numbers;Journal of Physics: Conference Series;2022-11-01
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