Estimation of aerodynamic coefficients of a non-slender delta wing under ground effect using artificial intelligence techniques
Author:
Publisher
Springer Science and Business Media LLC
Subject
Artificial Intelligence,Software
Link
https://link.springer.com/content/pdf/10.1007/s00521-022-07013-x.pdf
Reference66 articles.
1. Gursul I, Gordnier R, Visbal M (2005) Unsteady aerodynamics of nonslender delta wings. Prog Aerosp Sci 41:515–557. https://doi.org/10.1016/j.paerosci.2005.09.002
2. Ol MV, Gharib M (2003) Leading-edge vortex structure of nonslender delta wings at low reynolds number. AIAA J 41:16–26. https://doi.org/10.2514/2.1930
3. Gursul I, Allan MR, Badcock KJ (2005) Opportunities for the integrated use of measurements and computations for the understanding of delta wing aerodynamics. Aerosp Sci Technol 9:181–189. https://doi.org/10.1016/j.ast.2004.08.007
4. https://www.grc.nasa.gov/www/k12/airplane/liftco.html. Access date 08 June 2021, Adana
5. Kawazoe H, Morita S (2004) Ground effect on the dynamic characteristics of a wing-rock delta wing. In: 34th AIAA fluid dynamics conference and exhibit. https://doi.org/10.2514/6.2004-2352
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