1 |
Hagemann, G., Immich, H., Nguyen, T.V. and Dumnov, G.E., "Advanced Rocket Nozzles," Journal of Propulsion and Power, Vol. 14, No. 5, pp. 620-634, 1998.
DOI
|
2 |
Frey, M. and Hagemann, G., "Critical Assessment of Dual-Bell Nozzles," Journal of Propulsion and Power, Vol. 15, No. 1, pp. 137-143, 1999.
DOI
|
3 |
Genin, C., Stark, R., Haidn, O., Quering, K. and Frey, M., "Experimental and Numerical Study of Dual Bell Nozzle Flow," Progress in Flight Physics, Vol. 5, Torus Press, Moscow, pp. 363-376, Jun. 2013.
|
4 |
Taylor, N.V. and Hempsell C.M., "Throat Flow Modelling of Expansion Deflection Nozzles," Journal of the British Interplanetary Society, Vol. 57, pp. 242-250, 2004.
|
5 |
Schomberg, K., Olsen, J., Neely, A. and Doig, G., "Experimental Analysis of a Linear Expansion-Deflection Nozzle at Highly Overexpanded Conditions," 19th Australasian Fluid Mechanics Conference, Melbourne, Australia, pp. 74-77, Dec. 2014.
|
6 |
Schomberg, K., Doig, G. and Olsen, J., "Geometric Analysis of the Linear Expansion- Deflection Nozzle at Highly Overexpanded Study of an E-D Nozzle Geometric parameters for Altitude Compensation Flow Conditions," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014-4001, Cleveland, O.H., U.S.A., Jul. 2014.
|
7 |
Schneider, D., Genin, C., Stark, R. and Fromm, C.M., "Ariane 5 Performance Optimization Using Dual-Bell Nozzle Extension," Journal of Spacecraft and Rockets, Vol. 53, No. 4, pp. 743-750, 2016.
DOI
|
8 |
Kim, J., "Transient Characteristics and Performance Gain of Dual Bell Nozzle Based on developing Korean Launch Vehicle, KSLV-II," Master's Thesis, Department of Aerospace Engineering, Chungnam National University, Daejeon, Korea, 2017.
|
9 |
Goetz, A., Hagemann, G. and Kretschmer, J., "Advanced Upper Stage Propulsion Concept- The Expansion-Deflection Upper Stage," 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Az., U.S.A., AIAA 2005-3752, Jul. 2005.
|
10 |
Dzianis P., Koichi Y., Hidekazu K., Hiroaki T., Angelo P., Yoshinobu T., Tatsuya K., Kazuhiko Y. and Angelo P., "Control of Operation Mode Transition in Dual-Bell Nozzle with Film Cooling," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, U.S.A., AIAA 2010-6815, Jul. 2010.
|
11 |
Kim, H. and Koo, B., "A Study of the Flow Characteristics through a Supersonic Dual Bell Nozzle," Journal of The Korean Society for Propulsion Engineers, Vol. 4, No. 4, pp. 70-77, 2000.
|
12 |
Rajesh, G. and Kim, H., "A CFD study on the Supersonic Flow through a Dual Bell Nozzle," 38th KSPE Spring Conference, Gumi, Korea, pp. 324-330, May 2012.
|
13 |
Kim, J. and Huh, H., "Characteristics and Key Parameters of Dual Bell Nozzles of the DLR, Germany," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 43, No. 11, pp. 952-962, 2015.
DOI
|
14 |
Choi, J. and Huh, H., "Technology Review and Development Trends of Dual-Bell Nozzle for Altitude Compensation," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 43, No. 5, pp. 456-465, 2015.
DOI
|
15 |
Moon, T., Park, S., Choi, J. and Huh, H., "Numerical Study of Dual Bell Nozzle by applying the Concept of Expansion-Deflection Nozzle," KSPE Spring Conference, Jeju, Korea, pp. 679-681, May 2017.
|
16 |
Kim, J., Choi, J. and Huh, H., "Preliminary CFD Results of a Dual Bell Nozzle based on the KSLV-II," Journal of The Korean Society for Propulsion Engineers, Vol. 20, No. 6, pp. 18-28, 2016.
DOI
|
17 |
Choi, J. and Huh, H., "Numerical Study on Transition Characteristics of Dual Bell Nozzle with Expansion Ratio Fixed," Journal of The Korean Society for Propulsion Engineers, Vol. 21, No. 3, pp. 68-75, 2017.
DOI
|
18 |
Park, S., Moon, T. and Huh, H., "Study of an E-D Nozzle Geometric parameters for Altitude Compensation," KSAS Fall Conference, Jeju, Korea, pp. 1162-1163, Nov. 2016.
|
19 |
Moon, T., Park, S., Choi, J. and Huh, H., "Research Trends of an E-D Nozzle for Altitude Compensation," Aeronautical and Space Sciences, Vol. 45, No. 10, pp. 844-854, 2017.
|
20 |
International Civil Aviation Organization (ICAO), "Manual of the ICAO Standard Atmosphere: extended to 80 kilometres (262 500 feet)," ICAO-OACI-HKAO 7488/3, 1993.
|
21 |
Moon, Y. and Nam, C., "A Study of KSLV-II Engine System Development Test Program," KSPE Spring Conference, Busan, Korea, pp. 732-736, May 2013.
|
22 |
Choi, H., Han, Y., Ryu, C. and Kim, S., "Analytic Considerations of Liquid Rocket Engine Thrust Chamber Design for the KSLV-II," Journal of The Korean Society of Propulsion Engineers, Vol. 14, No. 4, pp. 71-80, 2010.
|
23 |
Kim, S., Moon, Y. and Park, T., "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.
|
24 |
Sutton, G.P., Rocket Propulsion Elements, 8th ed., John Wiley & Sons Inc., New Jersey, N.J., U.S.A., Ch. 3 and 5, 1992.
|
25 |
Im, J., Woo, S., So, Y., Kim, S., Lee, K. and Han, Y., "Design Point Hot-firing Test of Technology Demonstration Model for KSLV-II 75 tonf-class Combustion Chamber," KSPE Fall Conference, Gyeongju, Korea, pp. 697-700, Nov. 2015.
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