TY - JOUR
T1 - 喷气式客机层流翼气动设计综述
AU - Yang, Tihao
AU - Bai, Junqiang
AU - Duan, Zhuoyi
AU - Shi, Yayun
AU - Deng, Yiju
AU - Zhou, Zhu
N1 - Publisher Copyright:
© 2022 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
PY - 2022/11/25
Y1 - 2022/11/25
N2 - The laminar flow technology is the core technology for the future development of "green aviation", and its huge drag reduction potential makes it a research hotspot in the aviation field. This article starts from the physical characteristics of flow and the nature of transition phenomena of jet airliners, and expounds the realization principle and application scope of the NLF and HLFC technology. The global research status and development trend of the NLF/HLFC technology are reviewed. Focusing on the cutting-edge issues of the CFD-based laminar flow wing design technology, we systematically discuss the laminar flow from multiple levels of engineering application-oriented transition prediction methods, gradient-free/gradient-based optimization methods, uncertainty analysis and the robust optimization method. Meanwhile, the similarities and differences between the laminar flow wing aerodynamic design and full turbulent aerodynamic design are discussed, and the aerodynamic design theories of the NLF and HLFC wing are then sorted out. Finally, based on the development trend of the jet airliner technology, the problems faced by the laminar flow design technology are summarized, and the future development direction and suggestions for the aerodynamic optimization design technology of laminar flow wings are presented.
AB - The laminar flow technology is the core technology for the future development of "green aviation", and its huge drag reduction potential makes it a research hotspot in the aviation field. This article starts from the physical characteristics of flow and the nature of transition phenomena of jet airliners, and expounds the realization principle and application scope of the NLF and HLFC technology. The global research status and development trend of the NLF/HLFC technology are reviewed. Focusing on the cutting-edge issues of the CFD-based laminar flow wing design technology, we systematically discuss the laminar flow from multiple levels of engineering application-oriented transition prediction methods, gradient-free/gradient-based optimization methods, uncertainty analysis and the robust optimization method. Meanwhile, the similarities and differences between the laminar flow wing aerodynamic design and full turbulent aerodynamic design are discussed, and the aerodynamic design theories of the NLF and HLFC wing are then sorted out. Finally, based on the development trend of the jet airliner technology, the problems faced by the laminar flow design technology are summarized, and the future development direction and suggestions for the aerodynamic optimization design technology of laminar flow wings are presented.
KW - computational fluid dynamic
KW - drag reduction
KW - hybrid laminar flow
KW - natural laminar flow
KW - optimization design
UR - http://www.scopus.com/inward/record.url?scp=85143649076&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2022.27016
DO - 10.7527/S1000-6893.2022.27016
M3 - 文献综述
AN - SCOPUS:85143649076
SN - 1000-6893
VL - 43
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 11
M1 - 527016
ER -