| Citation: | YAO Shang-hong, LEI Yu-bing, ZHU Yan. Design and experimental research on 6 cm-diameters head-swirl micro-combustor[J]. Journal of Aerospace Power, 2009, 24(12): 2671-2677.
|
| [1] |
梁德旺,黄国平.厘米级微型涡轮喷气发动机主要研究进展[J].燃气涡轮试验与研究,2004,17(2):9213.LIANG Dewang,HUANG Guoping.Recent develop ment and key techniques of micro-turbine in centimeter size[J].Gas Turbine Experiment and Research,2004,17(2):9-13.(in Chinese)
|
| [2] |
Spadaccini C M,Mehra A,Zhang X,et al.High power density silicon combustion systems for micro gas turbine engines[J].Journal of Engineering for Gas Turbines and Power,2003,125:709-719.
|
| [3] |
曾川,王洪铭,单鹏.微涡喷发动机离心甩油盘环形折流燃烧室的设计与试验研究[J].航空动力学报,2003,18(1):92-96.ZENG Chuan,WAN G Hongming,SHAN Peng.The de-sign and study of the annular combustion chamber wit h cent rif ugal f uel injection[J].Journal of Aero space Pow-er,2003,18(1):92-96.(in Chinese)
|
| [4] |
熊庆荣,雷雨冰,黄国平,等.厘米级微型蒸发管式燃烧室性能试验研究[J].航空动力学报,2007,22(5):7332738.XION G Qingrong,LEI Yubing,HUANG Guoping,et al.Experimental research on a centimeter-scale micro com-bustor wit h vaporizing t ube[J].Journal of Aerospace Power,2007,22(5):733-738.(in Chinese)
|
| [5] |
Sullivan R E,Novick A S,Miles G A.Small gas turbine combustorprimary zone development[R].AIAA 1982-1159.
|
| [6] |
Sullivan R E,Sutton R,Miles G,et al.Application of 3D aerodynamic combustion model to combustor primary zone study[R].AIAA 1983-1265.
|
| [7] |
Prociw L A,Hu T C J,Hastings R R.Reducing tempera-t ure dist ribution factor(TDF)for advanced small gas t ur-bine engines[R].A GARD SEE N94-34431.
|
| [8] |
Martino P D,Cinque G,Colantuoni S,et al.Experimen-tal and computational result s from an advanced reverse-flow gas turbine combustor[R].AIAA 952-999.
|
| [9] |
Mc Guirk J J,Spencer A.Coupled and uncoupled CFD p re-diction of the characteristics of iet s from combustor air ad-mission port s[J].Journal of Engineering for Gas Turbines and Power,2001,123:327-332.
|
| [10] |
Spencer A,Mc Guirk J J.LDA measurements of feed an-nulus effects on combustor liner port flows[J].Journal of Fluids Engineering,2001,123:219-227.
|
| [11] |
Sturgess G J,Gogineni S.Influences of airblast-ato mizing fuel injector design on primary zone flame characteristics at blowout[R].AIAA 97-0269.
|
| [12] |
Sturgess G J,Gogineni S,Shouse D T,et al.Emissions and operability trades in the primary zones of gas turbine combustors[R].AIAA 96-2758.
|
| [13] |
Sturgess G J,Sloan D G,Lesmerises A L,et al.Design and develop ment of a research combustor for lean blow-outStudies[J].Journal of Engineering for Gas Turbines and Power,1992,114:13-19.
|
| [14] |
Ballal D R,Vangsness M D,Heneghan S P,et al.Studies of lean blowout in a research combustor[R].AGARD SEE N94-29246.
|
| [15] |
Rizk N K,Lefebvre A H.Spray characteristics of plain-jet airblast atomizers[R].ASME Paper 832GT2138,1983.
|
| [16] |
林宇震,刘俊,许全宏,等.微小“Г”型蒸发管在常压条件下蒸发率研究[J].航空动力学报,2006,21(5):843-847.LIN Yuzhen,LIU Jun,XU Quanhong,et al.study on vaporization rate of a miniГ2vaporizer under at mosp heric pressure condition[J].Journal of Aerospace Powe,2006,21(5):843-847.(in Chinese)
|
| [17] |
Khan Q S,Baek S W,Lee S Y.Effect of droplet initial di-ameter on droplet vaporization regimes for kerosene fuel droplet[R].AIAA 2007-1181.
|
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