| [1] |
Farhangi S,Yu T,Rojast L,et al.Gas-gas injector technology for full flow stage combustion cycle application[R].AIAA 1999-2757.
|
| [2] |
Jones J M,Nichols J T,Boyce W D,et al.Integrated powerhead demonstration:Full flow cycle development[R].Air Force Research Lab 4 DracoEdwards AFB,Aerojet PO Box 13222 Sacramento,William F.Sack,Boeing Defence & Space Group 6633 Canoga Ave Canoga Park,AFRL-PR-ED-TP-1998-003.
|
| [3] |
Davis J A,Campbell R L.Advantages of a full-flow staged combustion cycle engine system[R].AIAA 97-3318,1997.
|
| [4] |
Calhoon D,ho J,Kors D.Investigation of gaseous propellant combustion and associated injector-chamber design guide-lines[R].Aerojet Liquid Rocket Company,NASA CR-121234,Contract NAS3-13379,July 1973.
|
| [5] |
Muss J A,Johnson C W.Numerical cold flow and combustion characterization of swift coaxial injectors[R].AIAA 2003-124.
|
| [6] |
Foust M J,Deshpande M,Pal S,et al.Experimental and analytical characterization of a shear coaxial cornbusting GO2/GH2 flowfield[R].AIAA 1996-0646.
|
| [7] |
Tucker P K,Klemt M D,Smith T D,et al.Design of efficient GO2/GH2 injectors[R].A NASA,Industry and University Cooperative Effort,AIAA 1997.
|
| [8] |
Archambault M R,Talley D.Computational analysis of a single-element,shear-coaxial,GH2/GO2 engine[R].AIAA 2002-1088.
|
| [9] |
Marshall W MoPal S,Woodward R D,et al.Benchmark wall heat flux data for a GO2/GH2 single element combustor[R].AIAA-2005-3572.
|
| [10] |
Archambault M.Three-dimensional simulation of a gas/ gas,hydrogen/oxygen engine[R].AFRL-PR-ED-AB-2002-276.
|
| [11] |
Archamhault M,COhn R,Talley D.Computational analysis of a single-element,shear-coaxial,GH2/GO2 engine[R].AFRL-PR-ED-AB-2001-082.
|
| [12] |
Guo Biao,Jin Ping,Yang Lijun,et al.Experimental and numerical investigation of gas-gas injectors for full flow stage combustion cycle engine[R].AIAA-2005-3745.
|
| [13] |
王福军.计算流体动力学分析[M].北京:清华大学出版社,2004.
|