airfoil
airfoil
1. 3 Multi-objective optimization design of airfoil and wing,
5简化自适应机翼的气动外形优化设计
2. The advantages of FRP over other material, the rapid development of FW technology and the wide use of computer technology establish solid matter and technology foundation for the airfoil FW moulding.
FRP的优越性能、FW技术的迅猛发展以及计算机技术广泛的应用为机翼的FW成型奠定了物质和技术基础。
3. Effect of Gurney flaps on aerodynamical characters of single airfoil
Gurney襟翼对单段翼型动态气动特性的影响
4. PATRAN and the process in developing load module of airfoil FEM.
PATRAN进行二次开发程序编制的方法,以及开发机翼有限元模型加载模块的过程,为在msc.
5. Design of a Sine Driving Mechanism for the Dynamic Experiment of the Airfoil Model
一种用于翼型动态实验的正弦驱动机构设计
6. Bifurcation of Motions of an Airfoil in Incompressible Flow
不可压缩流中二元翼运动的分支问题
7. Analysis of Bifurcation of an Airfoil with an External Store in Incompressible Flow
不可压缩流中机翼外挂系统的分叉分析
8. Two pieces of foam are sandwiched onto the center piece and sanded to an airfoil shape.
两件是泡沫夹心到中心片和磨光的机翼形状。
9. The challenge of adequately cooling the nozzle guide vane directly downstream of the combustor is compounded by a complex vortical secondary flow at the junction of the endwall and the airfoil.
为了使空气在管道中能克服更大的阻抗，本研究设计管道风扇出口导流叶片，试图将流出叶轮之流体由迴旋流动导为直接流出风机，以达到提升风机性能的目的。
10. two-dimensional airfoil model
二元机翼模型
11. Sidewall Effects and Suction Technique in Two-Dimensional Transonic Airfoil Wind Tunnel Test
二元翼型风洞的侧壁干扰与抽气研究
12. Studies on Sidewall Effects in Two-Dimensional Airfoil Testing
二维翼型实验的侧壁影响研究
13. flow past a two-dimensional airfoil
二维翼型绕流
14. TWO DIMENSIONAL SIMULATION OF THE TRANSONIC FLOW OVER NACA 0012 AIRFOIL
二维翼型跨音速绕流的数值模拟
15. My seat near the airfoil, Java is over there.
今次坐机翼位，下面是爪哇岛。
16. Starting with airfoil 2, the pitching moment is increased from -.15 to -.25 to provide more aft loading and aft camber.
从翼型2俯仰时刻由原来的15年至今25年至今,以提供更多后部后部拱落.
17. Calculation of lift-drag characteristics of OAF and NACA63a312 airfoil at low speed using Jameson/TVD mixed scheme was carried out.
以Jameson/TVD混合格式对低速时的OAF和NACA63a312翼型的升阻特性进行了计算。
18. The bionic model could reduce air noise because the non-smooth shape has the characteristic of rectify flow around the airfoil and the control the turbulent breakaway .
仿生前缘非光滑形态具有整流及控制气流分离的特性，可减少由于翼表面气流压力脉动及涡流脱离引发的气流噪声。
19. Rogue Amoeba today announced the release of Airfoil 3.3.
仿生学单细胞虫今天宣布发型了3.3版机翼。
20. A small moveable airfoil on the side of the fuselage transmittng airplane angle relative to airstream for the stall warning system.
位于机身侧的可动小翼面，为失速警告系统传输飞机对气流的相对角度。
21. Aeroelastic Analysis of a Two-Dimensional Airfoil with Control Surface Freeplay Nonlinearity
具有操纵面间隙非线性二维翼段的气动弹性分析
22. The analytical results showed that Reynolds number and Mach number have a rather obvious effect on airfoil aerodynamic performances.
分析结果表明：雷诺数和马赫数对翼型气动性能有较大的影响。
23. Hierarchial Evolutionary Algorithms and Its Application in Transonic Airfoil Optimization in Aerodynamics
分级型进化算法及其在翼型跨声速气动优化中的应用
24. Visbal, M.R. and Shang, J.S., "Numerical Investigation of the Flow Structure Around A Rapidly Pitching Airfoil," AIAA Paper 87-1424, June. 1987.
刘泰然,"次音速非均匀流对二维翼剖面流场的影响"成功大学航太所硕士论文,1999年六月。
25. With the application of the above models, we research the influence of ground-effect on the flow near the surface of airfoil, the pressure distribution, and the moving of the vortices in the wake.
利用上述模型研究了地面对翼型表面流动和压力分布的影响，并对有地面存在条件下的尾涡发展规律进行了讨论。
26. It is one of approaches for unsteady inverse problems of oscillating airfoil to solve unsteady Bluer equations with finite difference method.
利用有限差分法解非定常欧拉方程是振荡机翼非定常气动反问题的一种求解方法。
27. How does the brake act on the paraglider airfoil?
刹车是如何作用于滑翔伞的翼型?
28. Somers,D.M.Design and experimental results for a natural-laminar-flow airfoil for general aviation applications.NASA TP 1861.June 1981.
华汉金.翼剖面优化理论在螺旋桨设计和减荷切削中的应用.船舶工程,2002(6).
29. A rotating airfoil on the tail of a single-rotor helicopter,keeps the helicopter from spinning in the direction opposite to the rotation of the main rotor.
单转子直升飞机尾部上的旋转机翼，防止直升飞机的旋转方向与主转子相反。
30. The ideal curvature in front part of designed blade may reasonably form shock position, so the shock loss is reduced greatly.Two kinds of airfoil are modified by means of this new method.
叶型入口段理想的曲率分布可以合理组织进口激波结构和位置，大幅降低激波损失。
31. Software for cascade airfoil design using aerodynamic hybrid method
叶型气动设计的杂交型方法计算软件
32. Near the midchord, the suction can provide a higher lift force for the airfoil.
吸气孔位置在翼面的中部附近增升效果较好;
33. Thus, it would be more advantageous to specify the velocity distribution from the outset and from that determine the airfoil shape.
因此,它会更有利,指明速度分布,从一开始就确定,从机翼形状.
34. The flow fields of an airfoil and simplified aircraft are calculated parallelly under MPI/PVM environmcent.
在MPI／PVM环境下用分区方法作了二维翼型和三维机翼绕流的并行计算。
35. Airfoil flutter is one of the important problems in aeroelasticity.
在气动弹性力学中,机翼振颤是一个非常典型的问题。
36. Finally the flow over two-element airfoil iscalculated.In the process of solving RANS equations, pressure-velocity coupling ishandled by using of SIMPLE algorithm.
在求解雷诺平均N-S方程的过程中，压力和速度的耦合是通过SIMPLE压力修正算法来实现的。
37. A new approach to modeling the unsteady rotor aerodynamic forces is established based on the insight into the nonuniform induced velocity distribution,inflow dynamics and unsteady airfoil behavior.
在考察非均匀诱速分布、入流动力学和非定常翼型性能的基础上，建立了一种模拟非定常旋翼气动力的新方法。
38. The thickness ratio appeared to have little effect on lift coefficient at zero angle of attack, since the angle of zero lift was largely determined by the airfoil camber.
在迎角为零时，由于零升力主要由机翼中弧线决定，相对厚度对升力几乎没有影响。
39. In this regard, several airfoil templates are given based on existing designs, eg, the SD7037 airfoil and others.
在这方面,有几个版本,基于现有翼型设计,例如,sd7037翼型等.
40. An unstructured grid was applied to the zone near the iced airfoil, whereas a structured grid was applied to save the storage and computational time.
在靠近积冰边界的内层采用了非结构网格，在非结构网格外采用结构化网格以节省存储空间和计算时间。
41. a hinged airfoil on the upper surface of an aircraft wing that is raised to reduce lift and increase drag
在飞机机翼上方的用来增加浮力减少拉力的装置
42. The flowfield around an airfoil with a spoiler is numerically simulated in a time-accurate manner using a 2D compressible Navier-Stokes solver.
基于2D可压N-S方程,对带扰流板的翼型绕流流场进行非定常数值模拟。
43. Genetic Algorithms for Airfoil Optimization Using Euler Equation Solver
基于Euler方程的翼型优化设计高效基因算法研究
44. Inverse design of airfoil based on variable-domain variational FEM
基于变域变分有限元的翼型反设计
45. In this paper, the optimization design of the transonic airfoil is performed by the Response Surface Methodology(RSM).
基于响应面方法进行了跨声速翼型的气动优化设计。
46. Transonic Euler Equation Airfoil Aerodynamic Optimization Based on Genetic Algorithms and Game Theory
基于基因算法与博奕论的翼型跨音速Euler方程气动优化
47. Optimization Design of Airfoil Based on Hybrid Genetic Algorithm and Compound Form Method
基于混合遗传算法和复合形法的翼型优化设计
48. MULTIOBJECTIVE OPTIMIZATION DESIGN OF A COMPRESSOR AIRFOIL USING EVOLUTIONARY ALGORITHMS
基于进化算法的压气机叶型多目标优化设计
49. Optimization Design of a High-Lift Airfoil at Low Reynold Numbers Based on Genetic Algorithm
基于遗传算法的低雷诺数高升力翼型的优化设计
50. Aerodynamic Properties of Circulation Control Airfoil with Multi-Slot Blowing
多喷口环量控制翼型流动的研究
51. High efficient evolutionary algorithms for multi-criteria optimization of multi-element airfoil in aerodynamics
多段翼型气动力优化设计的多标准高效进化算法
52. NUMERICAL SIMULATION OF VISCOUS FLOW FOR MULTI-ELEMENT AIRFOIL USING MULTI-BLOCK GRIDS
多段翼型粘性绕流多块网格数值模拟
53. Research on the Airfoil of Multi-blade Centrifugal Fan
多翼离心通风机叶片翼型的研究
54. Incremental Harmonic Balance Method for Airfoil Flutter With Multiple Strong Nonlinearities
多自由度强非线性颤振分析的增量谐波平衡法
55. STUDY ON PERFORMANCE OF AIR-FLOW MEASURING DEVICE WITH MULTI-DUCT AIRFOIL PROFILE
多风道翼型测风装置性能研究
56. Scanlan, R.H., and Tomko, J.J., (1971) “Airfoil and bridge deck flutter derivatives,” Journal of the Engineering Mechanics Division, ASCE, 97(EM6), 1717-1737.
姚忠达、杨永斌，(2000)，高速铁路车-桥互制理论，图文技术服务有限公司。
57. an airfoil mounted on the rear of a car to reduce lift at high speeds.
安装在汽车尾部的高速行使中减少升力的螺旋桨。
58. It appears that using NLF airfoil section can get a better aerodynamic efficiency and self-starting capability.
实验结果还表明，采用自然层流翼型的斜 轴式风力机比采用普通翼型的斜轴式风力机具有更好的气动效率和起 动能力。
59. The results detected the surface boundary layer transition positions by three techniques were excellent identical for two dimensional NACA-0012 airfoil model.
对二元NACA-0012翼型表面边界层转捩点位置测量，三种方法都给出了相吻合的结果。
60. A method has been derived for the determination of the downwash in the field of an airfoil extending through a circular jet.
对于采用钢桥面板系统做为主梁之细长型桥梁系统而言，往往采用侧向支撑系统以提高钢桥面板及主梁之抗扭转劲度。
61. The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
62. The wake survey cannot be used to measure the drag of stalled airfoil or of airfoils with flaps down.
尾流测量不能用来测量失连状态下的冀型或襟翼偏转后的翼型阻力。
63. Numerical Simulation of the Flowfield of an Airfoil with Spoiler
带扰流板翼型的流场数值模拟
64. Numerical Investigation of Unsteady Flow on Airfoil with a Spoiler
带扰流片的二维翼型非定常计算及分析
65. Adaptive airfoil with shape memory alloys
带有形状记忆致动器的自适应机翼
66. AN INVESTIGATION OF AIRFOIL FLUTTER CHARACTERISTICS WITH STRUCTURE NONLINEARITY AT TRANSONIC SPEED
带有结构非线性的跨音速翼型颤振特性研究
67. Experimental investigation of aerodynamics performance of multi-element airfoil with leading-edge slat
带缝翼多段翼型气动特性的实验研究
68. Mean geometric chord of airfoil
平均几何弦长
69. By using the Baldwin-Lomax turbulent model, the formation of the leading edge separation bubble, as well as the convection of vortex along the airfoil surface and unsteady phenomena of vortex are simulated at high angle of attack.
应用BaldwinLomax湍流二层代数模型模拟了大攻角时前缘分离涡的形成,旋涡对流及其非定常现象。
70. Aerodynamic Optimization Design of Cascade Airfoil Using Hybrid Evolutionary Algorithms
应用复合进化算法的叶栅气动优化设计方法的研究
71. Application of Hybrid Grid to Analyzing Complex Iced Airfoil Aerodynamic Performance
应用混合网格分析复杂积冰翼型气动性能
72. Provide an airfoil at the sill of the sash opening.It shall be mounted to provide a 1 inch slot above the hood interior counter top.
开口拉门处有一个翼面，安装时应在内部台面上留有1英寸的狭缝。
73. A slightly arched surface, as of a road, a ship's deck, an airfoil, or a snow ski.
弧面稍呈弧形的表面，如路面、船甲板、机翼面或滑雪板
74. The Effects of Elastic Vibration on the Flow Field near Stall-incidence of the Airfoil
弹性振动对翼型失速迎角附近流场的影响
75. As design studies progressed it was found that several airfoil shapes could be used to satisfy the new performance criteria.
当进行设计的研究工作后，发现有几种翼型可以用来满足新的性能指标。
76. In addition to JTB series Roots blower, our company also produces and sales low-noise DT tank centrifugal fan, T35/BT35, T30 axial fans, CF more airfoil centrifugal fan and axle roof ventilator.
我公司除生产销售JTB系列罗茨风机外，同时还生产销售DT低噪声柜式离心风机、T35/BT35、T30轴流风机、CF多翼型离心通风机及DWT型轴流式屋顶通风机等。
77. Adverse Lift on Airfoil with a Rapidly Deploying Spoiler
扰流片快速张开诱发的非定常升力过冲
78. Unsteady Flow Around Airfoil with a Rapidly Deploying Spoiler
扰流片快速张开诱发的非定常流动研究
79. To put the method in some perspective, it helpful to briefly outline the two general approaches to airfoil design.
把一些观点方法,它有助于扼要介绍两个一般方式翼型设计.
80. THE PIV EXPERIMENTAL RESEARCH TO INCREASE THE LIFT COEFFICIENT OF WINID TURBINE BLADE AIRFOIL
振荡射流提高风力机叶型升力的PIV实验
