A CFD Method for Simulation of Mixing and Combustion in High-Pressure LOX/Methane Rocket Engines
- 著者名:
- L. Cutrone ( Centro Italiano Ricerche Aerospaziali, CIRA, via Maiorise, Capua, Italy )
- F. Battista
- G. Ranuzzi
- S. Bonifacio ( Alstom Technology Center, Newbold Road, Rugby Warwickshire, United Kingdom )
- J. Steelant ( ESTEC-ESA, Noordwijk, The Netherlands )
- 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:
- 2008
- 発行年:
- 2008
- 通号:
- 2008-0949
- ペーパー番号:
- AIAA Paper 2008-0949
- 出版情報:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200801 [CD-ROM 2008 Disc 1]
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Effect of Combustion Process on Performance, Stability, and Durability of a LOX/Methane Rocket Engine
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 |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineering, Inc. |