Citation: | Lin Zhen, Wang Changhui, Liu Yu, et al. Flow separation and side-load in nozzle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(3): 307-310. (in Chinese) |
[1] Frey M,Hagemann G.Flow separation and side-load in rocket nozzles .AIAA 99-2815,1999 [2] Yasuhide W,Norio S,Koichi Y,et al.LE-7A engine nozzle flow separation phenomenon and the possibility of RSS suppression by the step inside the nozzle .AIAA 2004-4014,2004 [3] Menter F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA-Journal,1994,32(8):1598-1605 [4] Wang T S.Transient three-dimensional analysis of side load in liquid rocket engine nozzle .AIAA 2004-3681,2004 [5] Frey M,Hagemann G.Status of flow separation prediction in rocket nozzles .AIAA 98-3619,1998 [6] Kwan W,Stark R.Flow separation phenomena in subscale Ale rocket nozzles .AIAA 2002-4229,2002 [7] Nguyen A T,Deniau H,Girard S,et al.Wall pressure fluctuations in an over-expanded rocket nozzle .AIAA 2002-4001,2002 [8] Yasuhide Watanabe,Norio Sakazume,Masanori Tsuboi.LE-7A enine nozzle problems during the transient operations .AIAA 2002-3841,2002
|