forebody
forebody
1. Flow Visualization For An Unconventional Forebody
一个非常规前体机身的流动显示研究
2. This demonstrates that for propulsion-airframe integration, this genus of inlet would be advantageous in keeping the stability of boundary layer coming from the forebody.
一体化设计时，该进气道对保持前机体来流附面层的稳定性十分有利。
3. Waverider forebody
乘波前体
4. He has the head of arocodile, the forebody of a leapord, andhe hindquarters of a hippopotamus.
他 Tohno 已率领一个鳄鱼，前体一leapord和hindquarters一个河马。
5. forebody vortices control
前体涡控制
6. forebody drag
前体阻力
7. The method of lines is used to compute conical solutions for the sharp conical nose of the forebody.
前机身尖锥头部的锥型流场使用直线法求解。
8. A new method of quickly generating hypersonic waverider forebody configurations was developed.
发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。
9. Tzong-Shyng Leu, Pong-Jeu Lu, and Jeng-Ren Chang, " Application of Flexible Micro Balloon Actuators for Forebody Aerodynamic Control," International Symposium on Experimental Mechanics, December 2002.
吕宗行,陆鹏举,张政仁,"可桡性微泡致动器在前弹体气动力控制之应用,"中国航空航太学会,高雄,2002.
10. Forebody Vortices Control Using a Fast-Swinging Micro-Tip-Strake at High Angles of Attack
大攻角非对称流动的非定常弱扰动控制
11. An experimental study of pneumatic vortex flow control on high angle of attack forebody model
大迎角前机身模型上涡流气动控制的实验研究
12. Yao Opera is one of local operas of Tanhuang that belongs to Wu linguistic system with its forebody being “Yuyao Tanhuang”.
姚剧属吴语系滩簧类地方剧种之一，其前身为“余姚滩簧”。
13. The flush airdata sensing system is much better than the traditional airdata system, and it depends on the pressure sensors allocated on the forebody of aircraft to derive the airdata indirectly.
嵌入式大气数据传感(FADS)系统较之传统的大气数据系统有很大的优势，它依靠飞行器前端的压力传感器间接得到飞行大气数据。
14. Experimental and numerical investigation of a forward sweep sidewall compression scramjet inlet with forebody compression
带前体压缩的前掠侧压式进气道实验及数值研究
15. Computational investigation of slot blowing for fuselage forebody flow control
开缝吹气用于前机身流场控制的计算研究
16. Experiment Study of Aerodynamic Interactions of Projectile with Jet from Its Forebody
弹丸前体喷流的气动力干扰实验研究
17. The results demonstrate the accuracy of the present numerical procedure for investigating the aerodynamic heating on the forebody and the detailed structure of three-dimensional separations around the afterbody.
数值结果证实了本数值方法对研究再入物体的气动加热率的精确性，以及物体周围流场详细的三维流动分离结构是适用的。
18. The handling of complicated three-dimensional geometry models is described.The calculated results for forebody and biconics are presented.
本文描述了复杂的 三维几何模型的处理，并给出了前机身及双级锥的计算结果。
19. A numerical procedure is presented for computing the steady inviscid supersonic flow past forebody of an airplane.
本文提出了一种计算定常、无粘超音速绕前机身流场的数值方法。
20. L.E. Surber, Effect of forebody shape and shielding technique on 2 - D supersonic inlet performance, AIAA 75 - 1183
朱宇.前机身超音速绕流数值模拟研究:[硕士论文].北京:北京航空航天大学,1998
21. Study on the near-field aerodynamic characteristics of asymmetry spherical forebody of blunt body
球心非对称的钝圆头体近区绕流场气动特性分析研究
22. The results showed that the pressure drag coefficient increases rapidly with increasing upswept angle and contraction ratio respectively, and with decreasing forebody incidence.
研究结果表明，后体的压差阻力系数分别随上翘角、收缩比的增加及迎角的减小而明显增加；
23. slender forebody
细长体
24. Keywords Slender body;High AOA;Forebody vortices;Unsteady perturbation;Flow control;Flow field measurements;Seven holes probe;PIV;
细长旋成体;大攻角;非对称涡系;非定常小扰动;流动控制;流场测量;七孔探针测试技术;粒子图像测速技术;
25. Research of asymmetric vortex characteristic about forebody of slender wing and body
细长翼身组合体前体非对称涡特性研究
26. The vectoring jet effects are not only limited on the afterbody near the nozzle, but also on the forebody far away from the nozzles.
而喷流对附着流动和稳定旋涡流动的干扰效应最弱且集中于喷 口附近。
27. Optimized design of waverider forebody derived from asymmetric near-isentropic compression flow fields
轴对称近似等熵压缩流场的乘波前体优化设计
28. Forebody vortex control with miniature, rotatable nose-boom strakes
运用小型可旋转机头缘条边条进行前机身涡流控制
29. It is shown through this investigation that this kind of forebody has the potential to improve the lateral-direction stability of the ai rcraft at high angles of attack.
通过研究还表明，这类前体在改善大攻角横侧方向安定性方面具有很大的潜力。
30. To avoid the swing of forebody of robotic fish with single tail-fin,a kind of robotic fish with double tail-fin was designed and was used in SWATH.
针对单尾鳍摆动存在的机器鱼的摇艏问题,设计出双尾鳍仿鱼推进器,并将其应用于小水线面双体船,制作了仿生双尾推进的实验平台,在水池中进行了双尾推进试验研究。
31. AN EXPERIMENTAL STUDY ON FOREBODY VORTEX FLOW CONTROL TECHNIQUE USING COMBINED PERTURBATION
飞机大迎角非对称涡组合扰动主动控制研究
32. Forebody Compressibility Research of Hypersonic Vehicle
高超声速飞行器前体压缩性能研究
33. Opgitimization Method Research about the Forebody and Afterbody of Hypersonic Aircraft
高超音速飞行器前体优化设计方法研究
