References
- Rao, G.V.R., "Exhaust Nozzle Contours for Optimum Thrust," AIAA Journal of Jet Propulsion, Vol. 28, June, 1958, pp.377-383 https://doi.org/10.2514/8.7324
- Hoffman, J.D., "Design of Compressed Truncated Perfect Nozzles," AIAA Journal of Propulsion and Power, Vol. 3, No. 2, 1987, pp.150-156 https://doi.org/10.2514/3.22967
- Seddon, J., "The Flow Produced by Interaction of a Turbulent Boundary Layer with a Normal Shock Wave of Strength Sufficient to Cause Separation." Ph.D. Thesis, Ministry of Technology, 1967
- Lee, J.S., Kim, H.D., Setoguchi, T. and Matsuo, S., "Unsteady Shock-Flow Characteristics in an Over-Expanded Rocket Nozzle," Journal of Thermal Science, Vol. 19, No. 4, 2010, pp.332-336 https://doi.org/10.1007/s11630-010-0391-z
- Yonezawa, K., Yamashita, Y., Tsujimoto, Y., Watanabe, Y. and Yokota, K., "Effect of Contour on Flow Separation in Overexpanded Rocket Nozzles," Journal of Fluid Science and Technology, Vol. 2, No. 1, 2007, pp.97-108 https://doi.org/10.1299/jfst.2.97
- Nave, L.H. and Coffey, G.A., "Sea Levels Side Loads in High-Area-Ratio Rocket Engines," AIAA Paper 73-1284, 1973
- Chen, C. L., Chakravarthy, S. R., and Hung, C. M., "Numerical Investigation of Separated Nozzle Flows," AIAA Journal, Vol. 32, No. 9, 1994, pp.1836-1843 https://doi.org/10.2514/3.12181
- Frey, M., and Hagemann, G., "Restricted Shock Separation in Rocket Nozzle," Journal of Propulsion and Power, Vol. 16, No. 3, 2000, pp.478-484 https://doi.org/10.2514/2.5593
- Hagemann, G., Frey, M. and Koschel, W., "Appearance of Restricted Shock Separation in Rocket Nozzles," Journal of Propulsion and Power, Vol. 18, No. 3, 2002, pp.577-584 https://doi.org/10.2514/2.5971
- Hagemann, G., Frey, M., "Shock Pattern in the Plume of Rocket Nozzle: Needs for Design Consideration." Shock Waves Journal, Vol. 17, 2008, pp.387-395 https://doi.org/10.1007/s00193-008-0129-y
- 이종성, Vincent Lijo, 김희동, "과팽창 노즐에서 발생하는 충격파 박리 패턴의 천이에 관한 연구," 한국추진공학회지, 제14권, 제3호, 2010, pp.9-15
- Thi Nguyen, A. and Deniau, H., Girard, S. and Alziary de Roquefort, T., "Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle," Flow, Turbulence and Combustion, Vol. 71, 2003, pp.161-181
- Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp.1598-1605 https://doi.org/10.2514/3.12149
- Lee, J.S., Kim, H.D., Setoguchi, T. and Matsuo, S., "Experimental Visualization of Separation Shock Waves in an Over-Expanded Nozzle." Proc. 14th International Symposium on Flow Visualization, Daegu, 2010
- Nebbache, A. and Pilinski, C., "Pulsatory Phenomenon in a Thrust Optimized Contour Nozzle," Aerospace Science and Technology, Vol. 10, 2006, pp.295-308. https://doi.org/10.1016/j.ast.2005.07.002
- Lee, J.S., Kim, Lijo, V. and Kim, H.D., "A Computational Study on the Transition of the Shock-Boundary Layer Interaction in an Over-Expanded Nozzle," Proc. the Korean Society of Mechanical Engineers Spring Conference, 2010, pp.157-162