2009, Vol. 26(11): 114701-114701    DOI: 10.1088/0256-307X/26/11/114701
Influence of Rayleigh-Taylor Instability on Liquid Propellant Reorientation in a Low-Gravity Environment
LI Zhang-Guo1, LIU Qiu-Sheng1, LIU Rong1, HU Wei2, DENG Xin-Yu2
1Key Laboratory of Microgravity (National Microgravity Laboratory), Institute of Mechanics, Chinese Academy of Sciences, Beijing 1001902Beijing Institute of Astronautical Systems Engineering, Beijing 100076
收稿日期 2009-08-17  修回日期 1900-01-01
Supporting info

[1] Ostrach S 1982 Ann. Rev. Fluid Mech. 14 313

[2] Moran M E 2006 NASA/TM 2006-214264

[3] NASA Center 2005 NASA/TM 2005-214062

[4] Bradshaw R D and Kramer J L AIAA No 74-1076

[5] Long L H 1999 Missiles and Space Vehicles 239
1

[6] Long L H 1999 Missiles and Space Vehicles 240
1

[7] Sharp D H 1984 Physica D 12 3

[8] Rayleigh L 1883 Proc. London Math. Soc. 14 170

[9] Taylor G I 1950 Proc. Roy. Soc. London A 201
192

[10] Fu D X, Ma Y W and Li X L 2008 Chin. Phys. Lett.
25 188

[11] Zhang X and Tan D W 2009 Chin. Phys. Lett. 26
084703

[12] Scardovelli R and Zaleski S 1999 Ann. Rev. Mech.
31 567

[13] Hirt C W and Nichols B D 1981 J. Comput. Phys.
39 201

[14] Brackbill J U, Kothe D B and Zemach C 1992 J.
Comput. Phys. 100 335

[15] Bussmann M, Mostaghimi J and Chandra S 1999 Phys.
Fluids 11 1406