ROLLSTIN L.Measurement of inflight base pressure on an artillery-fired projectile[J].Journal of Spacecraft and Rockets,1990,27(1):5-6.
[2]
郭锡福.底部排气弹外弹道学[M].北京:国防工业出版社,1995.
[3]
GUO Xi-fu.Exterior ballistics of base bleed projectiles[M].Beijing:National Defence Industry Press,1995.(in Chinese)
[4]
BOWMAN J E,CLAYDEN W A.Cylindrical afterbodies in supersonic flow with gas ejection[J].AIAA Journal,1967,5(6):1 524-1 525.
[5]
MURTHY S N B,OSBORN J R.Aerodynamics of base combustion[M].Reston:AIAA,1976.
[6]
HERRIN J L,DUTTON J C.Supersonic base flow experiments in the near wake of a cylindrical afterbody[J].AIAA Journal,1994,32(1):77-83.
[7]
MATHUR T,DUTTON J C.Base bleed experiments with a cylindrical afterbody in supersonic flow[J].Journal of Spacecraft and Rockets,1996,33(1):30-37.
[8]
MATHUR T,DUTTON J C.Velocity and turbulence measurements in a supersonic base flow with mass bleed[J].AIAA Journal,1996,34(6):1 153-1 159.
[9]
SAHU J,NIETUBICZ C J,STEGER J L.Navier-Stokes computations of projectile base flow with and without base injection[J].AIAA Journal,1985,23(9):1 348-1 355.
[10]
GIBELING H J,BUGGELN R C.Projectile base bleed technology part Ⅰ:analysis and results,AD-A258 459[R].1992.
[11]
DANBERG J E,NIETUBICZ C J.Predicted flight performance of base bleed projectiles[J].Journal of Spacecraft and Rockets,1992,29(3):366-372.
[12]
梁德旺,王可.AUSM+格式的改进[J].空气动力学学报,2004,22(4):404-409.
[13]
LIANG De-wang,WANG Ke.Improvement of AUSM+scheme[J].Acta Aerodynamica Sinica,2004,22(4):404-409.(in Chinese)
[14]
YOON S,JAMESON A.Lower-upper symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations[J].AIAA Journal,1988,26(9):1 025-1 026.
WU Pin,ZHAO Run-xiang,GUO Xi-fu.Arc length method of grid generation and its application[J].Journal of Nanjing University of Science and Technology,2002,26(5):482-485.(in Chinese)
[17]
PRAMOD S,GRAHAM V C.Numerical investigations of supersonic base flows using DES[C]//AIAA Aerospace Sciences Meeting and Exhibit.Reno,Nevada:AIAA,2005.
[18]
SHIN J R,CHO D R,WON S H,et al.Hybrid RANS/LES study of base-bleed flows in supersonic mainstream[C]//AIAA International Space Planes and Hypersonic Systems and Technologies Conference.Dayton,Ohio:AIAA,2008.
[19]
MENTER F R.Two-equation eddy-viscosity turbulence models for engineering application[J].AIAA Journal,1994,32(8):1 598-1 605.