Conical Navier-Stokes Modeling of Forebody Vortex Symmetry Plasma Control
- 著者名:
- N. Malmuth ( Teledyne Scientific Company, Thousand Oaks, CA )
- S. Zakharov ( OIVTRAN, Moscow, Russia )
- A. Fedorov
- 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- シリーズ巻号:
- 2007
- 発行年:
- 2007
- 通号:
- 2007-0219
- ペーパー番号:
- AIAA Paper 2007-219
- 出版情報:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200702 [CD-ROM 2007 Disc 2]
- 資料種別:
- テクニカルペーパー
類似資料:
1
テクニカルペーパー
Modeling of Forebody Nose Vortex Symmetry Breaking Using Conical Navier-Stokes Solutions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
Parametric Studies of Hypersonic Laminar Flow Control Using a Porous Coating of Regular Microstructure
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |