[1] Anderson J D.Gasdynamic lasers:an introduction[M].New York:Academic Press,1976.

[2] Horkovich J A.Airborne laser pressure recovery system numerical simulations[C]//24th AIAA Plasmadynamics and Lasers Conference.1993:29.

[3] Merkli P E.Pressure recovery in rectangular constant area supersonic diffusers[J].AIAA J,1976,14(2):168-172.

[4] Anderson J D.Modern compressible flow:with historical perspective[M].3rd ed.New York:McGraw-Hill,2003.

[5] Lohn P D,Chan W R,Haflinger D E.COIL laser diffuser design[C]//32nd AIAA Plasmadynamics and Lasers Conference.2001.

[6] Acebal R.Evaluation of vaned diffuser performance applicable to chemical laser pressure recovery systems[C]//Proc of SPIE.1994,2119:59-67.

[7] FLUENT 6.1 Documentation[CP].USA:Fluent Inc,2003.

[8] 李桦,范晓樯,丁猛.超声速扩压器中激波串结构的数值模拟[J].国防科技大学学报,2002,24:18-21.(Li H,Fan X Q,Ding M.Numerical simulation of the shock train structure in the supersonic diffuser.Journal of National University of Defense Technology,2002,24:18-21)

[9] Kazuyasu M,Yoshiaki M,Heuy-dong K.Shock train and pseudo-shock phenomena in internal gas flows[J].Progress in Aerospace Sciences,1999,35:33-100.

[10] 蔡光明,刘军,宋影松,等.竖直隔板对COIL超扩段流场影响实验研究[J].强激光与粒子束,2003,15(8):729-732.(Cai G M,Liu J,Song Y S,et al.Experimental research of the influence of the vertical vane on the flow-field of COIL diffuser.High Power Laser and Particle Beams,2003,15(8):729-732)