Shock Wave Intelligent Prediction Method for Hypersonic Vehicle
Accurate prediction of shock wave position of hypersonic aircrafts can effectively improve the accuracy and efficiency of computational fluid dynamics (CFD) simulation. On the one hand, orthogonalization and densification of the grid near the shock wave of the hypersonic vehicle can effectively impr...
Main Authors: | Yuan-hao ZHU, Yue-qing WANG, Zhi-gong YANG, Guo-peng SUN, Wen-gang ZONG, Lei ZENG, Jian-qiang CHEN |
---|---|
Format: | Article |
Language: | zho |
Published: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2023-01-01
|
Series: | 气体物理 |
Subjects: | |
Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.0985 |
Similar Items
-
Numerical Investigation on Unsteady Shock Wave/Vortex/Turbulent Boundary Layer Interactions of a Hypersonic Vehicle during Its Shroud Separation
by: Pengcheng Cui, et al.
Published: (2022-10-01) -
Mesoscopic Kinetic Approach of Nonequilibrium Effects for Shock Waves
by: Ruofan Qiu, et al.
Published: (2024-02-01) -
Heat Transfer Characteristics of Gap Flows in Shock-Wave Interference Region of Hypersonic Vehicles
by: Zongyang LI, et al.
Published: (2024-03-01) -
Bow waves in hypersonic flow [filem gelung]
by: National Committee for Fluid Mechanics Films
Published: ([n.d) -
Shock waves : proceedings of the 26th International Symposium on Shock Waves, Gottingen, Germany, July 15-20, 2007 /
by: International Symposium on Shock Waves (26th : 2007 : Gottingen, Germany), et al.
Published: (2009)