Analysis of Swirl Coaxial Injecor with Backhole as an Acoustic Damper in Liquid Rocket Engines
- Author(s):
- Cha, E. ( Seoul National University, Seoul, South Korea )
- Kim, D.
- Kim, B.
- Yoon, Y.
- Bazarov, V.
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 41st
- Pub. Year:
- 2005
- No.:
- 2005-3748
- Paper no.:
- AIAA Paper 2005-3748
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200513 [CD-ROM 2005 Disc 13]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Performance Analysis of the Thrust Chamber in Liquid Rocket Engine Using Liquefied Natural Gas as a Fuel
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
The Characteristics of Swirl Coaxial Injector Under Varying Geometric and Environmental Conditions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Self-Pulsation Characteristics of a Swirl Coaxial Injector with Various Injection and Geometric Conditions
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Experimental Liquid Rocket Swirl Coaxial Injector Study Using Non-Intrusive Optical Techniques
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Effect of Geometry on the Liquid Film Thickness and Formation of Air Core in a Swirl Injector
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |