Numerical Simulation on Computational Model of Hypersonic Slip Flow

Article Preview

Abstract:

Three main computational models in hypersonic slip flow are derived and analyzed in detail and then compared by numerical simulation in which 2D cylinder hypersonic slip flow with Mach number 10 and Knudsen number 0.002, 0.01, 0.05, 0.25 are examined, results come out that the improved Maxwell slip model shows better applicability.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

241-244

Citation:

Online since:

May 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Li Hua, Tian Zhengyu. Numerical Simulation on The Effects of Hypersonic Slip Flow[C]. Near Space CFD Seminar, Beijing, (2010).

Google Scholar

[2] Kim K H, Kim C. Accurate Efficient and Monotomic Numerical Methods for Multi-Dimensional Compressible Flows Part I: Spatial Discretization[J]. Journal of Computational Physics, 208, (2005).

DOI: 10.1016/j.jcp.2005.02.021

Google Scholar

[3] Yoon S, Jameson A. Lower-Upper Symmetric Gauss-Sediel Method for the Euler and Navier-Stokes Equations [J]. AIAA Journal, 1988, 26(9).

DOI: 10.2514/3.10007

Google Scholar

[4] Lockerby D A, Reese J M, Emerson D R, Barber R W. Velocity Boundary Condition at Solid Walls in Rareedgas Calculations [J]. Physical Review E, 70(017303), (2004).

DOI: 10.1103/physreve.70.017303

Google Scholar

[5] Gokcen T, MacCormack R W. Nonequilibrium Effects for Hypersonic Transitional Flows Using Continuum Approach [R]. AIAA Paper 1989-0461, (1989).

DOI: 10.2514/6.1989-461

Google Scholar

[6] Cercignani C. Mathematical Methods in Kinetic Theory [M]. New York: Plenum Press, (1990).

Google Scholar

[7] Lockerby D A, Reese J M, Gallis M A. Capturing the Knudsen Layer in Continuum-Fluid Models of Nonequilibrium Gas Flows [J]. AIAA Journal, 43(6), (2005).

DOI: 10.2514/1.13530

Google Scholar

[8] Lofthouse A J, Scalabrin L C, Boyd I D. Velocity Slip and Temperature Jump in Hypersonic Aerothermodynamics [R]. AIAA 2007-208, (2007).

DOI: 10.2514/6.2007-208

Google Scholar