참고문헌 (15)

1. Ahlberg, J.H., Hamilton, S., Migdal, D. and Nilson, E.N., "Truncated Perfect Nozzles in Optimum Nozzle Design," ARS Journal, pp. 614-620, 1961. 

2. Rao, G.V.R., "Exhaust Nozzle Contour for Optimum Thrust," Jet Propulsion, Vol. 28, No. 6, pp. 372-382, 1958. 

3. Huzel, D.K. and Huang, D.H., "Modern Engineering for Design of Liquid-propellant Rocket Engines," Progress in Astronautics and Aeronautics, AIAA, Vol. 147, 1992. 

4. Hoffman, J.D., "Design of Compressed Truncated Perfect Nozzles," Jet Propulsion, Vol. 3, No. 2, pp. 150-156, 1987. 

   상세보기

5. Vuillermoz, P., Weiland, C., Hagemann, G., Aupoix, B., Grosdemange, H. and Bigert, M., "Nozzle Design and Optimization," AIAA paper, pp. 469-492, 2004. 

6. Cai, G., Fang, J., Xu, X. and Liu, M., "Performance Prediction and Optimization for Liquid Rocket Engine Nozzle," Aerospace Science and Technology, Vol. 11, pp. 155-162, 2007. 

   상세보기

7. Kim, I., Lee, J.W., Choi, M.K. and Kwon, S., "Optimum Nozzle Angle of a Micro Solid Propellant Thruster," Nanoscale and Microscale Thermophysical Engineering, Vol. 15, No. 3, pp. 165-178, 2011. 

   상세보기

8. Kim, S.K., Joh, M., Choi, H.S. and Park, T.S., "Multidisciplinary Simulation of a Regeneratively Cooled Thrust Chamber of Liquid Rocket Engine: Turbulent Combustion and Nozzle Flow," International Journal of Heat and Mass Transfer, Vol. 70, pp. 1066-1077, 2014. 

   상세보기

9. Kim, S.K., Moon, Y.W. and Park, T.S., "Development of Chemical Equilibrium CFD Code for Performance Prediction and Optimum Design of LRE Thrust Chamber," Journal of the Korean Society of Propulsion Engineers, Vol. 9, No. 1, pp. 1-8, 2005. 

10. Wang, Q.D., Fang, Y.M., Wang, F. and Li, X.Y. "Skeletal Mechanism Generation for High-temperature Oxidation of Kerosene Surrogates," Combustion and Flame, Vol. 159, pp. 91-102, 2012. 

    상세보기

11. ANSYS Fluent User Guide 13.0. 

12. Sutton, G.P. and Biblarz, O., Rocket Propulsion Elements, 6th ed., John Wiley & Sons Inc., New York, U.S.A., 1992. 

13. Ostlund, J. and Muhammad-Klingmann, B. "Supersonic Flow Separation with Application to Rocket Engine Nozzles," Applied Mechanics Reviews, Vol. 58, pp. 143-177, 2005. 

    상세보기

14. Reid, R.C., Prausnitz, J.M. and Poling, B.E., The Properties of Gases & Liquids, 4th ed., McGraw-Hill Book Company, New York, U.S.A., 1986. 

15. Rao, G.V.R., "Approximation of Optimum Thrust Nozzle Contour," ARS Joutrnal, Vol. 30, No. 6, pp. 561, 1960. 

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