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XFOIL vs CFD performance predictions for high lift low Reynolds number airfoils

  • Published:2016-05 Issue: Volume:52 Page:207-214
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Morgado J.,Vizinho R.,Silvestre M.A.R.,Páscoa J.C.

Funder

Seventh Framework Programme

C-MAST – Center for Mechanical and Aerospace Sciences and Technologies, Portuguese Foundation for Science and Technology Research Unit No. 151

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Optimization design study of low-Reynolds-number high-lift airfoils for the high-efficiency propeller of low-dynamic vehicles in stratosphere;Ma;Sci. China, Technol. Sci.,2010

2. The rebirth of airships;Prentice;J. Transp. Res. Forum,2005

3. A critical review of propulsion concepts for modern airships;Ilieva;Cent. Eur. J. Eng.,2012

4. Multibody advanced airship for transport;Dumas,2011

5. Parametric study of a high altitude airship according to the multi-body concept for advanced airship transport – MAAT;Morgado,2012

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