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Nonlinear vortex flow control for high-angle-of-attack maneuvering

โœ Scribed by J.M. Buffington; R.J. Adams


Publisher
Elsevier Science
Year
1995
Tongue
English
Weight
1019 KB
Volume
3
Category
Article
ISSN
0967-0661

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Numerical solution for complete aircraft
โœ E Qin; Yang Guowei; Li Fengwei ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 788 KB

In this paper, the conformal mapping technique combined with the algebraic method is used to generate the unified body fitted orthonormal O-H mesh for fighter-type aircraft. The flow field and aerodynamic characteristics of complete aircraft's subsonictransonic-supersonic flow at angles of attack up