Aerodynamic Design for Three- Dimensional Multi- lifting Surfaces at Transonic Flow
Autor: | Wichmann Georg, Zhong-yin Zhang, Qing-zhen Yang, Streit Thomas, Yong Zheng |
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Rok vydání: | 2006 |
Předmět: |
Surface (mathematics)
Engineering business.industry Mechanical Engineering Aerodynamic potential-flow code Aerospace Engineering Mechanical engineering Aerodynamics transonic flow aerodynamic design Convergence (routing) Software design iterative residual correction Subsonic and transonic wind tunnel Aerospace engineering multi-lifting surfaces business canard wing Choked flow Transonic |
Zdroj: | Chinese Journal of Aeronautics. 19:24-30 |
ISSN: | 1000-9361 |
DOI: | 10.1016/s1000-9361(11)60263-x |
Popis: | An aerodynamic design method and corresponding codes are developed for three dimensional multi-lifting surfaces at transonic flow. It is based on the “iterative residual correction” concept that is successfully used for transonic wing design and subsonic multi-lifting surface design. The up wind scheme is introduced into governing equations of multi-lifting surface design method and automatically acted when supersonic flow appears on the surface. A series of interface codes are programmed, including a target- pressure modification tool. Using the improved inverse aerodynamic design code, T A U code and interface codes, the transonic multi-lifting aerodynamic design software system is founded. Two cases of canardwing configuration have been performed to validate the method and codes. The results show that the convergence of analysis/design iteration is very good at higher speed transonic flow. |
Databáze: | OpenAIRE |
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