Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Ao-ping PENG"'
Publikováno v:
气体物理, Vol 8, Iss 5, Pp 38-45 (2023)
Counter-flow engines are often used for aircraft slowing or separating. In order to study the interaction between the counter-flow jets and free stream at high altitudes, the rarefied flow driven by two counter-flow jets and hypersonic free stream wa
Externí odkaz:
https://doaj.org/article/d0cd46252c1b4d789f624e5f06cfd31b
Publikováno v:
Advances in Aerodynamics, Vol 1, Iss 1, Pp 1-21 (2019)
Abstract How to solve the hypersonic aerothermodynamics around large-scale uncontrolled spacecraft during falling disintegrated process from outer space to earth, is the key to resolve the problems of the uncontrolled Tiangong-No.1 spacecraft reentry
Externí odkaz:
https://doaj.org/article/8f62f1c7d046431ab9504ddc49256f7a
Based on the Direct Simulation Monte Carlo (DSMC) method, an unsteady flow, which is caused by the interaction of two counter-flow jets with a hypersonic free stream, is constructed and simulated in the rarefied regime for the flight altitude of 90 k
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47c44ef125f41afce521750022570d18
https://doi.org/10.21203/rs.3.rs-2585272/v1
https://doi.org/10.21203/rs.3.rs-2585272/v1
Publikováno v:
International Journal for Numerical Methods in Fluids. 92:922-949
Publikováno v:
International Journal of Heat and Mass Transfer. 132:484-497
Numerical investigation of some mixing enhancement strategies based on the traditional transverse injection technique proposed in recent years was carried out by means of the three-dimensional Reynolds-average Navier–Stokes (RANS) equations coupled
Publikováno v:
Physics of Fluids. 34:046111
A Boltzmann model equation (kinetic model) involving the chemical reaction of a multicomponent gaseous mixture is derived based on Groppi's work [“A Bhatnagar–Gross–Krook-type approach for chemically reacting gas mixtures,” Phys. Fluids 16, 4
Publikováno v:
Physics of Fluids. 33:126114
Publikováno v:
Computers & Fluids. 155:50-61
The unsteady process of rarefied jet flows expanding into a vacuum is numerically solved by the Gas-Kinetic Unified Algorithm (GKUA) based on the Boltzmann model equations. The discrete velocity ordinate method (DVOM) is adopted to discretize the vel
Publikováno v:
Advances in Aerodynamics, Vol 1, Iss 1, Pp 1-21 (2019)
How to solve the hypersonic aerothermodynamics around large-scale uncontrolled spacecraft during falling disintegrated process from outer space to earth, is the key to resolve the problems of the uncontrolled Tiangong-No.1 spacecraft reentry crash. T
Publikováno v:
31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS: RGD31.
How to solve the hypersonic aerothermodynamics around large-scale uncontrolled spacecraft during falling disintegrating process from outer space to earth, is the key to predict the flight track of the end-of-life spacecraft reentry crash. To study ae