Unstructured Dynamic Mesh for Large Movement and Deformation.

Unstructured Dynamic Mesh for Large Movement and Deformation.

著者名:

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:

2002

発行年:

2002

通号:

2002-0122

ペーパー番号:

2002-0122

総ページ数:

11

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:	ZA00001706
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	40th
会議開催地:	Reno, NV
会議開催年:	2002.01.14-2002.01.17
論文注記:	40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 14-17 January 2002

類似資料:

1 テクニカルペーパー Simulation of Aircraft Response to Control Surface Deflection Using Unstructured Dynamic Grids Murayama, M., Togashi, F., Nakahashi, K., Matsushima, K., Kato, T. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Flap-Edge Flowfield and Noise in Civil Transport Aircraft Model M. Kuroda, Y. Yokokawa, M. Murayama, K. Nakahashi, Y. Fukunishi American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Viscous Flow Computations of Aircraft with Changing Control Surface Deflection Using Unstructured Grids Murayama, M., Ito, Y., Nakahashi, K., Matsushima, K., Iwamiya, T. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー NUMERICAL SIMULATION OF VORTICAL FLOWS USING VORTICITY CONFINEMENT COUPLED WITH UNSTRUCTURED GRID Murayama,Mitsuhiro, Nakahashi,Kazuhiro, Obayashi,Shigeru American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Comparison Study of Drag Prediction for the 3rd CFD Drag Prediction Workshop by Structured and Unstructured Mesh Method (Invited) M. Murayama, K. Yamamoto American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Out-of-Core Streamline Visualization on Large Unstructured Meshes Shyh-Ueng, Kuang, Sikorski, K., Kwan-Ma, Liu National Aeronautics and Space Adminstration
4 テクニカルペーパー Validation of Flows on High-Lift Configurations by Structured and Unstructured Mesh Method Murayama, M., Yamamoto, K., Kobayashi, K. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー High-Density Mesh Flow Computations with Pre-/Post-Data Compressions Nakahashi, K. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー An Approach to Generate High Quality Unstructured Hybrid Meshes Y. Ito, A. Shih, B. Soni, K. Nakahashi American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Validation of CFD Capability for Supersonic Transport Analysis Using NEXST-1 Flight Test Results M. Umeda, K. Takenaka, K. Hatanaka, D. Hirayama, W. Yamazaki, K. Matsushima,, K. Nakahashi American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Design and Aerodynanics of Lift Enhancement Control for a Single Element Airfoil Shiokawa, M., Matsushima, K., Nakahashi, K. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー FLOW SIMULATION OF FLAPPING WINGS OF AN INSECT USING OVERSET UNSTRUCTURED GRID TOGASHI,Fumiya, ITO,Yasushi, MURAYAMA,Mitsuhiro, NAKAHASHI,Kazuhiro, KATO,Takuma American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12