| Citation: | XIE Ye-ping, SHANG Shou-tang, LI Jian-rong, SHI Lei. Optimization of aero-engine nozzle control schedule under the maximum dry thrust condition based on installation performance[J]. Journal of Aerospace Power, 2014, 29(1): 175-180. doi: 10.13224/j.cnki.jasp.2014.01.023
|
| [1] |
Lee C G T, Edwin E Jr.Experimental and analytical investigagion of axisymmetric supersonic cruise nozzle geometry at Mach numbers from 0.6 to 1.3[R].NASA TP-1953, 1981.
|
| [2] |
陶增元, 王如根.飞机推进系统总体设计[M].北京:国防工业出版社, 2002.
|
| [3] |
Sellers J F, Daniel C J.DYN GEN:a program for calculating steady and transient performance of turbojet and turbofan engines[R].NASA TN-D-7901, 1975.
|
| [4] |
黄家骅, 冯国泰, 于廷臣.涡喷发动机涡轮改型匹配的数值仿真[J].推进技术, 2005, 26(2):151-154. HUANG Jiahua, FENG Guotai, YU Tingchen, et al.Numerical simulation of redesigned turbine matching in turbojet engine[J].Journal of Propulsion Technology, 2005, 26(2):151-154.(in Chinese)
|
| [5] |
Follen G, Aubuchon M.Numerical zooming between a NPSS engine system simulation and a one-dimensional high compressor analysis code[R].NASA TM-2000-209913, 2000.
|
| [6] |
John L, Gregory F, Cynthia N, et al.2001 numerical propulsion system simulation review[R].NASA TM-2002-211197, 2002.
|
| [7] |
Evans A L, Pollen G, Naiman C, et al.Numerical propulsion system simulation's national cycle program[R].AIAA 98-3113, 1998.
|
| [8] |
陈玉春, 黄兴, 高本兵, 等.发动机总体与尾喷管三维并行设计研究[J].航空动力学报, 2007, 22(10):1695-1699. CHEN Yuchun, HUANG Xing, GAO Benbing, et al.Parallel design of turbo engine and three-dimensional nozzle[J].Journal of Aerospace Power, 2007, 22(10):1695-1699.(in Chinese)
|
| [9] |
金捷, 赵景芸, 张明恒, 等.轴对称矢量喷管内流特性的模型试验[J].推进技术, 2005, 26(2):144-146. JIN Jie, ZHAO Jingyun, ZHANG Mingheng, et al.Experimental investigation of static internal performance for an axisymmetric vectoring thrust nozzle[J].Journal of Propulsion Technology, 2005, 26(2):144-146.(in Chinese)
|
| [10] |
邵万仁.流路参数对收扩喷管内流特性影响的数值研究[J].航空动力学报, 2012, 27(10):2356-2363. SHAO Wanren.Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle[J].Journal of Aerospace Power, 2012, 27(10):2356-2363.(in Chinese)
|
| [11] |
张群锋, 吕志咏.轴对称矢量喷管外流对内流干扰研究[J].航空动力学报, 2003, 18(3):322-327. ZHANG Qunfeng, LÜ Zhiyong.Effect of outer flow on internal performance of axisymmetric vectoring nozzle[J].Journal of Aerospace Power, 2003, 18(3):322-327.(in Chinese)
|
| [12] |
黄宏艳, 王强.过膨胀状态下轴对称收-扩喷管内外流场计算及分析[J].航空动力学报, 2007, 22(7):1069-1073. HUANG Hongyan, WANG Qiang.Numerical investigation on internal and external flows for axisymmetric convergent-divergent nozzles on over-expansion state[J]. Journal of Aerospace Power, 2007, 22(7):1069-1073.(in Chinese)
|
| [13] |
Carson J R.Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90.NASA TM-4506, 1994.
|
| [14] |
罗静, 王强, 额日其太.轴对称矢量喷管内流特性的不同湍流模型计算[J].推进技术, 2003, 24(4):326-329. LUO Jing, WANG Qiang, Eriqitai.Computation for the effect of turbulence models on internal performance for axisymmetric vectoring exhaust nozzles[J].Journal of Propulsion Technology, 2003, 24(4):326-329.(in Chinese)
|
| [15] |
刘大响, 叶培梁, 胡骏, 等.航空燃气涡轮发动机稳定性设计与评定技术[M].北京:航空工业出版社, 2004.
|
DownLoad: