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[1]雷震.唐云龙.VXI数据采集系统的建立及其应用[J].火箭推进,2008,34(05):54-58.
 Lei Zhen,Tang Yunlong.Establishment and application of VXI data acquisition system[J].Journal of Rocket Propulsion,2008,34(05):54-58.
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VXI数据采集系统的建立及其应用

参考文献/References:

[l]Holland Scott D.An Experimental Parametric Study of Geometric,Reynolds Number,and Ratio of Specific Heats Effects in‰e--dimensional Sidewall Compression Scramjet Inlets al Mach 6[R].AIAA93-0740.
[2]Siebenhaar A,Bulman M J.The Role of the Strutjet Engine in New Gbbal and Space Markets[R].IAF-98一S. 5.04.
[3]3 Falempin F,Goldfeld M,Nestoulia R,et a1.Evaluation of a Variable Geometry Inlet for Dual Mode Ramjet[R]. AIAA一2002—5232.
[4]Michael K Smart,Carl A Trexler.Mach 4 Performance of a Fixed-geometry Hypersonic Inlet with Rectangular-toelliptical Shape Transition[R].AIAA一2003—12.
[5]丛敏.阿连特技术系统公司试验高超声速发动机[J].飞 航导弹.2007,(10):42
[6]蔡元虎,张建东,壬占学.TBCC发动机用进气道设 计及沿飞行轨迹斜板角度优化分析[J].西北工业大学 学报.2007,25(5):615--619.

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备注/Memo

收稿日期:2008—03—28;修回日期:2008--05—30。 作者简介:雷震(1971一),男,高级工程师,研究领域为液体火箭发动机试验技术。

更新日期/Last Update: 1900-01-01