TY - JOUR
T1 - The application of the implicit scheme of the multiscale discrete velocity method for three-dimensional flows of diatomic gas in all flow regimes
AU - Zhang, Qingdian
AU - Zhong, Chengwen
AU - Zhuo, Congshan
AU - Mu, Junlei
AU - Jin, Hao
AU - Liu, Sha
N1 - Publisher Copyright:
© 2025 Elsevier Masson SAS
PY - 2025/10
Y1 - 2025/10
N2 - This paper presents the development of an implicit multiscale discrete velocity method, which is applicable to three-dimensional flows of diatomic gas in all flow regimes. The Boltzmann-Rykov model equation serves as the fundamental governing equation for this implicit method. By implicitly solving this equation along with its corresponding macroscopic adjoint equations, the efficiency in addressing problems across all flow regimes is significantly enhanced. To reduce the additional memory consumption associated with implicit solutions, this paper utilizes point-relaxation symmetric Gauss-Seidel iteration to solve the governing equations. Moreover, inspired by the construction philosophy of the discrete unified gas kinetic scheme, a multiscale interface flux is formulated, and the macroscopic flux is decomposed into equilibrium and non-equilibrium components, thereby enhancing the stability of the algorithm. Through a series of three-dimensional flow cases, including lid-driven cavity flow, flow around a sphere, flow around an Apollo 6 capsule, flow around a blunted-cone, and flow around an X-38 vehicle, this paper comprehensively validates the accuracy of the proposed implicit algorithm in managing all flow regime problems and demonstrates an efficiency improvement of one to two orders of magnitude compared to the corresponding explicit algorithm.
AB - This paper presents the development of an implicit multiscale discrete velocity method, which is applicable to three-dimensional flows of diatomic gas in all flow regimes. The Boltzmann-Rykov model equation serves as the fundamental governing equation for this implicit method. By implicitly solving this equation along with its corresponding macroscopic adjoint equations, the efficiency in addressing problems across all flow regimes is significantly enhanced. To reduce the additional memory consumption associated with implicit solutions, this paper utilizes point-relaxation symmetric Gauss-Seidel iteration to solve the governing equations. Moreover, inspired by the construction philosophy of the discrete unified gas kinetic scheme, a multiscale interface flux is formulated, and the macroscopic flux is decomposed into equilibrium and non-equilibrium components, thereby enhancing the stability of the algorithm. Through a series of three-dimensional flow cases, including lid-driven cavity flow, flow around a sphere, flow around an Apollo 6 capsule, flow around a blunted-cone, and flow around an X-38 vehicle, this paper comprehensively validates the accuracy of the proposed implicit algorithm in managing all flow regime problems and demonstrates an efficiency improvement of one to two orders of magnitude compared to the corresponding explicit algorithm.
KW - All flow regimes
KW - Discrete velocity method
KW - Implicit method
KW - Three-dimensional flows
UR - http://www.scopus.com/inward/record.url?scp=105008973330&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2025.110489
DO - 10.1016/j.ast.2025.110489
M3 - 文章
AN - SCOPUS:105008973330
SN - 1270-9638
VL - 165
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 110489
ER -