Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows

Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows

著者名:

Kawai, S. ( University of Tokyo, Tokyo, Japan )
Fujii, K. ( Japan Aerospace Exploration Agency, Kanagawa, Japan )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Fluid Dynamics Conference

シリーズ巻号:

35th

発行年:

2005

通号:

2005-5156

ペーパー番号:

AIAA Paper 2005-5156

出版情報:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200511 [CD-ROM 2005 Disc 11]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001628
シリーズID:	PA00000147
会議名:	AIAA Fluid Dynamics Conference and Exhibit
回次:	35th
会議開催地:	Toronto, Ontario, Canada
会議開催年:	2005.06.06-2005.06.09

類似資料:

1 テクニカルペーパー Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Large-Eddy Simulation of Compressible Transitional Boundary Layer S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Computational Study of a Supersonic Base Flow Using LES/RANS Hybrid Methodology Kawai,S., Fujii,K. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Flow Field Analysis of the Base Region of Axisymmetric Aerospike Nozzles Ito,T., Fujii,K. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Computational Analysis of Characteristics of Mach Wave Sources in Supersonic Free-Jets T. Nonomura, K. Fujii American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Aerodynamic Characteristics of a Lifting-Body-Type Reentry Vehicle at Transonic Speeds M. Kurita, K. Nakakita, K. Mitsuo, Y. Yamamoto, S. Watanabe, K. Fujii, H. Kawato American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Comparative advantages of high-order schemes for subsonic, transonic, and supersonic flows C. Safta, K. Alabi, F. Ladeinde American Institute of Aeronautics and Astronautics	10 テクニカルペーパー COMPUTATION OF 3-DIMENSIONAL VISCOUS TRANSONIC FLOWS USING THE LU-ADI FACTORED SCHEME Fujii, K. National Aeronautics and Space Administration
5 テクニカルペーパー Prediction of a Thin-Airfoil Stall Phenomenon Using LES/RANS Hybrid Methodology with Compact Difference Scheme Kawai, S., Fujii, K. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー TranAir: A full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations. … Johnson, F. T., Samant, S. S., Bieterman, M. B., Melvin, R. G., Young, D. P., Bussoletti, J. E., Hilmes, C. L. National Aeronautics and Space Adminstration
6 テクニカルペーパー Compact Differencing and Filtering Schemes for Large-Eddy Simulation of Compressible Transitional Boundary Layer S. Kawai, K. Fujii American Institute of Aeronautics and Astronautics	12 テクニカルペーパー TranAir: A full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations. … Johnson, F. T., Samant, S. S., Bieterman, M. B., Melvin, R. G., Young, D. P., Bussoletti, J. E., Hilmes, C. L. National Aeronautics and Space Adminstration

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