1 |
Hutt, J.J. and Rocker, M., Liquid Rocket Engine Combustion Instability, Vol. 169 Progress in Astronautics and Aeronautics, AIAA Inc., Washington, DC, USA, Ch. 12, 1995.
|
2 |
Baer M. R. and Mitchell C. E., "A Theoretical Evaluation of Rigid Baffles in Suppression of Combustion Instability," Colorado State University, Fort Collins, Colorado, USA, NASA CR-134986, 1976.
|
3 |
Mitchell, C. E., Liquid Rocket Engine Combustion Instability, Vol. 169 Progress in Astronautics and Aeronautics, AIAA Inc., Washington, DC, USA, Ch. 15, 1995.
|
4 |
Nguyen, T. V., "Computer code for use in high frequency combustion stability analyses," Aerojet TechSystems Company, Thermodynamic analysis report 9980:1807, 1988.
|
5 |
Kobayashi, K., Daimon, Y., Iizuka, N., Tamura, H., Mitani, T., and Onodera, T., "Studies on Combustion Instability for Liquid Propellant Rocket Engines," 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Diego, CA, USA, AIAA, July-Aug. 2011.
|
6 |
Schulze, M. and Sattelmayer, T., "A Comparison of Time and Frequency Domain Descriptions of High Frequency Acoustics in Rocket Engines with Focus on Dome Coupling," Aerospace Science and Technology, Vol. 45, pp. 165-173, 2015.
DOI
|
7 |
Sattelmayer, T., Schmid, M., and Schulze, M., "Impact of Injector Mass Flow Fluctuations on Combustion Dynamics in Liquid Engines," Journal of Spacecraft and Rockets, Vol. 52, No. 5, pp. 1417-1429, 2015.
DOI
|
8 |
Yi, Y., Hong, M., and Lee, S.Y., "Experimental Study on the Merged Angle of Mixed-Interaction Regions of Sprays from Two Pressure-Swirl Injectors," Journal of ILASS-KOREA, Vol. 16, No. 4, pp. 195-200, 2011.
|
9 |
Bazarov, V., and Yang. V., "Liquid -Propellant Rocket Engine Injector Dynamics," Journal of Propulsion and Power, Vol. 14, No. 5, pp. 797-806, 1998.
DOI
|
10 |
Kim, D., Im, J., Koh, Hl, and Yoon, Y., "Effect of Ambient Gas Density on Spray Characteristics of Swirling Liquid Sheets," Journal of Propulsion and Power, Vol 23, No.3, pp.603-611, 2007.
DOI
|
11 |
Fang, J., "Application of Combustion Time-lag Theory to Combustion Stability Analysis of Liquid and Gaseous Propellant Rocket Engines", 22nd Aerospace Science Meeting, Reno, NV USA, AIAA paper 84-0510, 09-12 Jan. 1984.
|