[1] |
Guy R W, Rogers R C, Puster R L, et al. The NASA Langley scramjet test complex[R]. AIAA-1996-3243, 1996.
|
[2] |
Powell E S, Stallings D W. A review of test medium contamination effects on test article combustion processes[R]. AIAA-1998-0557, 1998.
|
[3] |
Pellett G L, Bruno C, Chinitz W. Review of air vitiation effects on scramjet ignition and flameholding combustion processes[R]. AIAA-2002-3880, 2002.
|
[4] |
Edelman R B, Spadaccini L J. Theoretical effects of vitiated air contamination on ground testing of hypersonic airbreathing engines[J]. Jouranl of Spacecraft and Rockets, 1969, 6(12):1442-1447. doi: 10.2514/3.29844
|
[5] |
Tirres C, Bradley M, Morrison C, et al. A flow quality analysis for future hypersonic vehicle testing[R]. AIAA-2002-2706, 2002.
|
[6] |
Engelund W C, Holland S D, Cockrell C E Jr, et al. Aerodynamic data base development for the Hyper-X air frame-integrated scramjet propulsion experiments[J]. Journal of Spacecraft and Rockets, 2001, 38(6):803-810. doi: 10.2514/2.3768
|
[7] |
Garrand D. A plan for defining the effects of test medium on hypersonic propulsion systems-where do we start[C]//Proc of JANNAF 25th Airbreathing Propulsion Subcommittee, 37th Combustion Subcommittee and 1st Modeling & Simulation Subcommittee Joint Meeting. 2008.
|
[8] |
Goyne C P, Cresci D. Hy-V program overview and status[R]. AIAA-2008-2577, 2008.
|
[9] |
Goyne C P, McDaniel J C Jr, Krauss R H, et al. Test gas vitiation effects in a dual-mode scramjet combustion[J]. Journal of Propulsion and Power, 2007, 23(3):559-565. doi: 10.2514/1.24663
|
[10] |
Haw W L, Goyne C P, Rockwell R D, et al. Experiment study of vitiation effects on scramjet mode transition[J]. Journal of Propulsion and Power, 2011, 27(2):506-508. doi: 10.2514/1.49090
|
[11] |
Rockwell R D, Goyne C P, Haw W L, et al. Experimental study of test-medium vitiation effects on dual-mode scramjet performance[J]. Journal of Propulsion and Power, 2011, 27(5):1135-1142. doi: 10.2514/1.B34180
|
[12] |
Rockwell R D, Goyne C P, Haw W L, et al. Measurement of water vapor levels for investigating vitiation effects on scramjet performance[J]. Journal of Propulsion and Power, 2011, 27(6):1315-1317. doi: 10.2514/1.B34270
|
[13] |
Noda J, Tomioka S, Izumikwa M, et al. Estimation of enthalpy effects in direct connect dual-mode combustor[J]. Journal of Thermal Science and Technology, 2011, 6(2):289-296. doi: 10.1299/jtst.6.289
|
[14] |
Noda J, Masuya G, Tomioka S, et al. Comparison of dual-mode combustor performance with various heating methods[R]. AIAA-2011-6087, 2011.
|
[15] |
Mitani T, Hiraiwa T, Sato S, et al. Comparison of scramjet engine performance in Mach 6 vitiated and storage-heated air[J]. Journal of Propulsion and Power, 1997, 13(5):635-642. doi: 10.2514/2.5228
|
[16] |
Hiraiwa T, Sato S, Tomioka S, et al. Testing of a scramjet engine model in Mach 6 vitiated air flow[R]. AIAA-1997-0292, 1997.
|
[17] |
Ingenito A. Theoretical investigation of air vitiation effects on hydrogen fuelled scramjet performance[J]. International Journal of Hydrogen Energy, 2015, 40(6):2862-2870. doi: 10.1016/j.ijhydene.2014.12.014
|
[18] |
邵菊香, 谈宁馨, 刘伟雄, 等.空气污染组分H2O和CO2对乙烯燃烧性能的影响(Ⅱ)-反应机理和动力学模拟[J].物理化学学报, 2010, 26(2):270-276. doi: 10.3866/PKU.WHXB20100140Shao J X, Tan N X, Liu W X, et al. Influence of H2O and CO2 in air on the combustion of ethylene(Ⅱ)-reaction mechanism and kinetics simulation[J]. Acta Physico-Chimica Sinica, 2010, 26(2):270-276. doi: 10.3866/PKU.WHXB20100140
|
[19] |
梁金虎, 王苏, 张灿, 等. H2O/CO2污染对RP-3航空煤油着火特性的影响[J].推进技术, 2015, 36(3):336-344. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=tjjs201503003Liang J H, Wang S, Zhang C, et al. Effects of H2O and CO2 on ignition characteristics of RP-3 aviation kerosene[J]. Journal of Propulsion Technology, 2015, 36(3):336-344. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=tjjs201503003
|
[20] |
Würmel J, Silke E L, Curran H J, et al. The effect of diluent gases on ignition delay times in the shock tube and in the rapid compression machine[J]. Combustion and Flame, 2007, 151(1-2):289-302. doi: 10.1016/j.combustflame.2007.06.010
|