Numerical simulation of the BGK-Burnett equations for hypersonic blunt body flows using the kinetic wave-particle flux splitting algorithm

Numerical simulation of the BGK-Burnett equations for hypersonic blunt body flows using the kinetic wave-particle flux splitting algorithm

Author(s):

Balakrishnan, Ramesh ( Department of Aerospace Engineering, Wichita State University )
Agarwal, Ramesh K. ( Department of Aerospace Engineering, Wichita State University )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1998

Pub. Year:

1998

No.:

98-0848

Paper no.:

98-0848

Page(from):

1

Page(to):

25

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050859
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1998.01.12-1998.01.15
Note for article:	36th Aerospace Sciences Meeting & Exhibit, January 12-15, 1998/Reno, NV

Similar Items:

1 Technical Paper A kinetic theory based scheme for the numerical solution of the BGK-Burnett equations for hypersonic flows in the continuum-transition regime Balakrishnan, Ramesh, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics	7 Technical Paper NUMERICAL SIMULATION OF COMPRESSIBLE VISCOUS MHD FLOWS FOR REDUCING SUPERSONIC DRAG OF BLUNT BODIES Agarwal, Ramesh K., Augustinus, Justin American Institute of Aeronautics and Astronautics
2 Technical Paper A comparative study of augmented Burnett and BGK-Burnett equations for computing hypersonic blunt body flow Yun, Keon-Young, Agarwal, Ramesh K., Balakrishnan, Ramesh American Institute of Aeronautics and Astronautics	8 Technical Paper Higher-order distribution functions, BGK-Burnett equations and Boltzmann's H-theorem Balakrishnan, Ramesh, Agarwal, Ramesh K., Yun, Keon-Young American Institute of Aeronautics and Astronautics
3 Technical Paper A HIGHER-ORDER KINETIC WAVE/PARTICLE FLUX-SPLITTING ALGORITHM FOR THE EULER EQUATIONS Reksoprodjo, Heru, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics	9 Technical Paper Numerical Simulations of Hypersonic Magnetogasdynamic Flows Over Blunt Bodies Damevin, H.-M., Hoffmann, K.A. American Institute of Aeronautics and Astronautics
4 Technical Paper A higher-order kinetic wave/particle flux-splitting algorithm for the Euler equations Reksoprodjo, Heru, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics	10 Technical Paper Computation of Hypersonic Flow of a diatomic Gas in Rotational Nonequlibrium Past a Blunt Body Using the Generalized Boltzmann Equation R. Chen, R. Agarwal, F. Cheremisin American Institute of Aeronautics and Astronautics
5 Technical Paper Computations of Hypersonic Flow of a diatomic gas in rotational non-equilibrium past 3D blunt bodies using the generalized Boltzmann equation Wilson, Christopher D., Agarwal, Ramesh K., Tcheremissine, Felix G. American Institute of Aeronautics and Astronautics	11 Technical Paper A comparative study of several higher-order kinetic formulations beyond navier-stokes for computing the shock structure Balakrishnan, Ramesh, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics
6 Technical Paper Numerical simulation of compressible viscous MHD flows for reducing supersonic drag of blunt bodies Agarwal, Ramesh K., Augustinus, Justin American Institute of Aeronautics and Astronautics	12 Technical Paper A COMPARATIVE STUDY OF SEVERAL HIGHER-ORDER KINETIC FORMULATIONS BEYOND NAVIER-STOKES FOR COMPUTING THE SHOCK STRUCTURE Balakrishnan, Ramesh, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12