1 |
Nebbache, A. and Pilinski, C., "Pulsatory Phenomenon in a Thrust Optimized Contour Nozzle," Aerospace Science and Technology, Vol. 10, 2006, pp.295-308
DOI
ScienceOn
|
2 |
Nasuti, F. and Onofri, M., "Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles," AIAA Journal, Vol 36, No. 5, 1998, pp.809-815
DOI
ScienceOn
|
3 |
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
DOI
|
4 |
Hoffman, J.D., "Design of Compressed Truncated Perfect Nozzles," AIAA Journal of Propulsion and Power, Vol. 3, No. 2, 1987, pp.150-156
DOI
ScienceOn
|
5 |
Hadjadj A., Onofri M., "Nozzle Flow Separation," Shock Wave Journal, Vol. 19, No. 3, 2009, pp.163-169
DOI
ScienceOn
|
6 |
Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp.1598-1605
DOI
ScienceOn
|
7 |
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
DOI
ScienceOn
|
8 |
Frey, M. and Hagemann, G., "Restricted Shock Separation in Rocket Nozzles," AIAA Journal of Propulsion and Power, Vol. 16, No. 3, 2000, pp.478-484
DOI
ScienceOn
|
9 |
Nave, L.H. and Coffey, G.A., "Sea Levels Side Loads in High-Area-Ratio Rocket Engines," AIAA Paper 73-1284, 1973
|
10 |
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
DOI
|
11 |
Nagdewe, S.P., 이종성, 김희동, "로켓노즐에 서 발생하는 횡력변동에 관한 연구," 한국추진공학회 춘계학술대회 논문집, 2009, pp.315-319
|
12 |
Yonezawa, K., Morimoto, T., Tsujimoto, Y., Watanabe, Y. and Yokota, K., "A Study of an Asymmetric Flow in an Overexpanded Rocket Nozzle," Journal of Fluid Science and Technology, Vol. 2, No. 2, 2007, pp.400-409
DOI
|
13 |
Rao, G.V.R., "Exhaust Nozzle Contours for Optimum Thrust," AIAA Journal of Jet Propulsion, Vol. 28, June, 1958, pp.377-383
DOI
|