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Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow

โœ Scribed by Patil, Mayuresh J.; Hodges, Dewey H.; S. Cesnik, Carlos E.


Book ID
120811022
Publisher
American Institute of Aeronautics and Astronautics
Year
2000
Tongue
English
Weight
382 KB
Volume
37
Category
Article
ISSN
0021-8669

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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