Open Access
| Issue |
JNWPU
Volume 39, Number 4, August 2021
|
|
|---|---|---|
| Page(s) | 753 - 760 | |
| DOI | https://doi.org/10.1051/jnwpu/20213940753 | |
| Published online | 23 September 2021 | |
- Li Weiwei. Turbomachinery aerodynamic shape optimization approach using adjoint method and its applications for blade detail design[D]. Beijing: University of Chinese Academy of Sciences, 2013 (in Chinese) [Google Scholar]
- Li Jing. The research and application of aerodynamic shape design method for high performance aircraft[D]. Xi'an: Northwestern Polytechnical University, 2014 (in Chinese) [Google Scholar]
- Xu Shengguan. A study of aerodynamic shape optimization based on Kriging surrogate models[M]. Nanjing: Nanjing University of Aerodynamics and Astronautics, 2012 (in Chinese) [Google Scholar]
- Yu Guangyuan. Aerodynamic design of large curvature diffuser channel by using adjoint method based on FFD technique[M]. Nanjing: Nanjing University of Aerodynamics and Astronautics, 2014 (in Chinese) [Google Scholar]
- Jameson A. Aerodynamic design via control theory[J]. Journal of Scientific Computing, 1988(3): 233–260 [Google Scholar]
- Kim S, Alonso J J, Jameson A. A gradient accuracy study for the adjoin-based Navier-Stokes design method[R]. AIAA-1999-16201 [Google Scholar]
- Nadarajah S, Jameson A. Studies of the continuous and discrete adjoint approaches to viscous automatic aerodynamic shape optimization[R], AIAA-2001-2530 [Google Scholar]
- Jameson A. Efficient aerodynamic shape optimization[R]. AIAA-2004-4396 [Google Scholar]
- Kim S, Alonso J J, Jameson A. Multi-element high-lift configuration design optimization using viscous continuous adjoint method[J]. Journal of Aircraft, 2004, 41(5): 1083–1096 [Google Scholar]
- Jameson A, Martinelli L, Cliff S, et al. Aerodynamic shape optimization of transonic and supersonic aircraft configurations[R]. AIAA-2005-1013 [Google Scholar]
- Lyu Z, Martins J R R A. Aerodynamic design optimization studies of a blended-wing-body aircraft[J]. Journal of Aircraft, 2014, 51(5): 1604–1617 [Article] [Google Scholar]
- Yang Xudong. Aerodynamic optimization method research based on control theory[D]. Xi'an: Northwestern Polytechnical University, 2002 (in Chinese) [Google Scholar]
- Xiong Juntao. Aerodynamic shape optimization design based on adjoint approach using Navier-Stokes equations[D]. Xi'an: Northwestern Polytechnical University, 2007 (in Chinese) [Google Scholar]
- Liu Xiaodong, Yang Xudong. Multi-point aerodynamic inverse design method of wing based on adjoint method[J]. Aeronautical Computing Technique, 2012, 42(5): 60–64 [Article] (in Chinese) [Google Scholar]
- Feng Zhenping, Li Haitao, Song Liming, et al. Aerodynamic inverse design optimization for turbine cascades based on control theory[J]. Scientia Sinca Technologica, 2013, 43(3): 257–273 [Article] (in Chinese) [Google Scholar]
- Bai Junqiang, Lei Ruiwu, Yang Tihao, et al. Progress of adjoint-based aerodynamic optimization design for large civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(1): 522642 [Article] (in Chinese) [Google Scholar]
- Liu Shaowei, Bai Junqiang, Yu Peixun, et al. Aerodynamic optimization design on supersonic transports considering sonic boom intensity[J]. Journal of Northwestern Polytechnical University, 2020, 38(2): 271–278 [Article] [Article] (in Chinese) [Google Scholar]
- Wang Hufeng, Bai Junqiang. Design essentials research of the flying-wing configuration[J]. Science Technology and Engineering, 2009, 9(12): 1671–1819 [Article] (in Chinese) [Google Scholar]
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