本文数值模拟喉部半高为34μm的二维微喷管,分别分析了固定进口及固定喉部尺度下扩张角、扩张比以及滑移边界条件对微喷管性能的影响,发现最佳半扩张角在20°~22°之间,而最佳扩张比为7.为了比较壁面滑移条件对计算结果影响,分别数值模拟了喉部尺寸为68μm和6.8 μm的微喷管,发现Kn<0.001时,滑移边界条件对数值模拟结果较小;而0.002<Kn<0.045时,壁面滑移对流场和微喷口推力性能有较大影响.
参考文献
[1] | C Rossi;T Do Conto;D Esteve et al.Design, Fabrication and Modelling of MEMS-based Microthrusters for Space Application[J].Smart Materials and Structures,2001,10(06):1156-1162. |
[2] | M R Wang;Z X Li .Numerical Simulations on Performance of MEMS-Based Nozzles at Moderate or Low Temperatures[J].Microfluidics and Nanofluidics,2004,1(01):62-70. |
[3] | J Mueller.Thruster Options for Microspacecraft: a Review and Evaluation of Existing Hardware and Emerging Techonogies[A].AIAA,1997:3058-3063. |
[4] | Bayt RL .Analysis, Fabrication and Testing of a MEMS Based Micropropulsion System[D].MIT Cambridge:MA USA,1999. |
[5] | G Sutherland;M Maes .A Review of Microrocket Technology: 10-6 to 1 lbf Thrust[J].Journal of Spacecraft and Rockets,1996,3(08):1153-1163. |
[6] | RL Bayt;KS Breuer .Fabrication and Testing of Mcironsized Cold-Gas Thruster, In Micropropulsion for Small Spacecraft[J].Progress in Astronautics and Aeronautics,2000,187(02):381-397. |
[7] | Markelov G N;Ivanov M S .Numerical Study of 2D/3D Micronozzle Flows[J].Int AIP Conference Proceedings,2001,585:539-546. |
[8] | Bayt R L;Breuer K.Viscous Effects in Supersonic MEMS-Fabricated Micronozzles[A].Anaheim CA ASME,New York,1998:117-123. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%