[1]LU F K. Prospects for detonations in propulsion [C]// Pro- ceedings of the 9th International Symposium on Experi- mental and Computational Aerothermodynamics of Inter- nal Flows. Gyeongju, Korea: ISAIF, 2009: 8-11.
[2]OSTRANDER M J, HYDE J C, YOUNG M F, et al. Stan- ding oblique detonation wave engine performance, AIAA 1987-2002 [R]. USA: AIAA, 1987.
[3]SISLIAN J P. Propulsive performance of hypersonic oblique detonation wave and shock-induced combustion ramjets[J]. Journal of Propulsion and Power, 2001, 17(3): 599-604.
[4]FUSINA G, PARENT B. Stability of standing oblique de- tonation waves, AIAA2004-1125 [R]. USA: AIAA, 2004.
[5]HARRIS P G. Structure of conical oblique detonation waves[C]// 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. [S.l.]: AIAA, 2008.
[6]FUSINA G, PARENT B. Numerical study of structure and stability of oblique detonation waves [C]// 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: AIAA, 2004:11-22.
[7]CARRIER G F. Nonintrusive stabilization of a conical detonation wave for supersonic combustion[J]. Combustion and Flame, 1995, 103(4): 281-295.
[8]LEE J H S. Initiation of gaseous detonation[J]. Annual Review of Physical Chemistry, 1977, 28: 75-104.
[9]GROSS R A. A study of supersonic combustion[J]. Journal of the Aero/Space Sciences, 1960, 27(7): 517-524.
[10]RUBINS P M. Shock-induced combus- tion with oblique shocks, comparison of experiment and kinetic calculations[J]. AIAA Journal, 1963, 1(12): 2778-2784.
[11]LEHR H F. Experiments on shock induced combustion [J]. Astron. Acta., 1972, 17(4): 589-597.
[12]CHOI J Y, JEUNG I S, YOON Y. Validation of CFD al- gorithms for unsteady shock-induced combustion, AIAA 98-3217[R]. USA: AIAA, 1998.
[13]KAMIYAMA Y. Flow features of shock-in- duced combustion around cylindrical projectiles[J]. Sym- po- sium (International) on Combustion, 2000, 28: 671-677.
[14]KANESHIGE M J, SHEPHERD J E. Oblique detonation stabilized on a hypervelocity projectile[J]. Symposium (International) on Combustion, 1996， 26(2): 3015-3022.
[15]VIGUIER C, GOURARA A, DESBORDES D. Three-di- mensional structure of stabilization of oblique detonation wave in hypersonic flow[J]. Symposium (International) on Combustion, 1998, 27: 2207-2214.
[16]VIGUIER C. Onset of oblique detonation waves: com- parison between experimental and numerical results for hydrogen-air mixtures[J]. Symposium (International) on Combustion, 1996, 26(2): 3023-3031.
[17]MORRIS C I. Combined schlieren and OH PLIF imaging study of ram accelerator flowfields, AIAA 98-0244[R]. USA: AIAA, 1998.
[18]LI C, KAILASANATH K, ORAN E. Effects of boundary layers on oblique-detonation structures, AIAA 1993-0450 [R]. USA: AIAA, 1993.
[19]PAPALEXANDRIS M V. A numerical study of wedge- induced detonations[J]. Combustion and Flame, 2000, 120 (4): 526-538.
[20]KASAHARA J, ARAL T, MATSUO A, et al. Experimen- tal investigations of steady-state oblique detonation waves generated around hypersonic projectiles, AIAA 2001-1800 [R]. USA: AIAA, 2001.
[21]GRISMER M J, POWERST J M. Calculations for steady propagation of a generic ram accelerator configuration[J]. Journal of Propulsion and Power, 1995, 11(1): 111-121.
[22]FAN H Y. Numerical study of reactive flow past a wedge in a channel, AIAA 2005-1168[R]. USA: AIAA, 2005.
[23]CHOI J Y. Unstable combus- tion induced by oblique shock waves at the non-attach- ing condition of the oblique detonation wave[J]. Pro- ceedings of the Combustion Institute, 2009, 32(2): 2387-2396.
[24]FUSINA G, SISLIAN J P, PARENT B. Computational study of formation and stability of standing oblique de- tonation waves, AIAA 2004-1125[R]. USA: AIAA, 2004.
[25]POWERS J M, STEWARTT D S. Approximate solutions for oblique detonations in the hypersonic limit[J]. AIAA Journal, 1992, 30(3): 55-66.
[26]ASHFORD S A, EMANUEL G. Wave angle for oblique detonation waves[J]. Shock Waves, 1994, 3(4): 327-329.
[27]ISHII K. Initiation and propagation of detonation waves in combustible high speed flows [J]. Proceedings of the Combustion Institute, 2009, 32: 2323-2330.
[28]LEFEBVRE M H, FUJIWARA T. Numerical modeling of combustion processes induced by a supersonic conical blunt body[J]. Combustion and Flame, 1995, 100(1-2): 85-93.
[29]STEWART D S, KASIMOV A R. State of detonation stability theory and its application to propulsion[J]. Journal of Propulsion and Power, 2006, 22(6): 1230.
[30]CHOI J Y. Capturing unstable wrinkled oblique detonation wave front by Hi-Fi numerical simulation, AIAA 2006-5100[R]. USA: AIAA, 2006.
[31]HIGGINS A J. Ram accelerators: outstanding issues and new directions[J]. Journal of Propulsion and Power, 2006, 22(6): 1170-1177.
[32]HE L. An analysis of the quenching phenomenon and low frequency instability in detonations induced by blunt projectiles, AIAA-97-0806[R]. USA: AIAA, 1997.
[33]DAIMON Y, MATSUO A, KASAHARA J. Wave struc- ture and unsteadiness of stabilized oblique detonation waves around hypersonic projectile, AIAA 2007-1171[R]. USA: AIAA, 2007.
[34]WALTER M A T, FIGUEIRA L F. Numerical study of detonation stabilization by finite length wedges[J]. AIAA Journal, 2006, 44(2): 353-361.