A kinetic theory based scheme for the numerical solution of the BGK-Burnett equations for hypersonic flows in the continuum-transition regime

A kinetic theory based scheme for the numerical solution of the BGK-Burnett equations for hypersonic flows in the continuum-transition regime

著者名:

Balakrishnan, Ramesh ( Wichita State University )
Agarwal, Ramesh K.

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

1996

発行年:

1996

通号:

96-0602

ペーパー番号:

96-0602

開始ページ:

1

終了ページ:

16

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050843
シリーズID:	PA00000138
会議名:	Aerospace Sciences Meeting and Exhibit
回次:	34th
会議開催地:	Reno, NV
会議開催年:	1996.01.15-1996.01.18
論文注記:	34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV

類似資料:

1 テクニカルペーパー Numerical simulation of the BGK-Burnett equations for hypersonic blunt body flows using the kinetic wave-particle flux splitting algorithm Balakrishnan, Ramesh, Agarwal, Ramesh K. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー 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
2 テクニカルペーパー NUMERICAL SOLUTION OF 3-D AUGMENTED BURNETT EQUATIONS FOR HYPERSONIC FLOW IN CONTINUUM-TRANSITION REGIME Yun, K., Agarwal, R. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A NOVEL SET OF SECOND-ORDER HYDRODYNAMIC EQUATIONS FOR FLOWS IN CONTINUUM-TRANSITION REGIME Agarwal,R.K. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー 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	9 テクニカルペーパー Implicit Kinetic Schemes for Euler Equations Reksoprodjo,H.S.Raharjaya, Agarwal,Ramesh K. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Beyond Navier Stokes: Burnett equations for flow simulations in continuum-transition regime Agarwal, R., Yun, K., Balakrishnan, R. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー 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
5 テクニカルペーパー BEYOND NAVIER STOKES: BURNETT EQUATIONS FOR FLOW SIMULATIONS IN CONTINUUM-TRANSITION REGIME Agarwal, R., Yun, K., Balakrishnan, R. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー 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 テクニカルペーパー DEVELOPMENT OF AN OBJECT-ORIENTED THREE-DIMENSIONAL BURNETT EQUATIONS SOLVER FOR COMPUTING HYPERSONIC FLOWS IN CONTINUUM-TRANSITION REGIME Swargam,S., Agarwal,R.K., Yun,K.-Y. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー NUMERICAL INVESTIGATION OF REAL GAS EFFECTS ON MAGNETOHYDRODYNAMIC HYPERSONIC FLOWS Gupta,Anurag, Agarwal,Ramesh K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12