Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics
- 著者名:
D. Salgues ( Pennsylvania State University, University Park, PA ) A. Mouis S. Lee D. Kalitan S. Pal R. Santoro - 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:
- 2006
- 発行年:
- 2006
- 通号:
- 2006-0757
- ペーパー番号:
- AIAA Paper 2006-757
- 出版情報:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200604 [CD-ROM 2006 Disc 4]
- 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
Experimental Liquid Rocket Swirl Coaxial Injector Study Using Non-Intrusive Optical Techniques
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Experimental Study of Transverse Combustion Instabilities in a Multi-Element, Rectangular Rocket Chamber
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity
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 |
10
テクニカルペーパー
Combustion Stability Assessment of Double Swirl Coaxial Injectors Using Simulant Propellants
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Effects of LOx Post Recess on the Combustion Characteristics for Bi-Swirl Coaxial Injector
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Experimental investigation of oxygen rich LOX/GH2 combustion using linewise Raman imaging
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Effect of Swirl Injector Design and Other Important Parameters on Gas Turbine Combustion
American Institute of Aeronautics and Astronautics |