forebody
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n.
船身前半部，弹体前部；前体；
权威例句
ForebodyFlow Control over a Conical Forebody Using Duty-Cycled Plasma Actuators
Proportional Control of Asymmetric Forebody Vortices
Closed-Loop Missile Yaw Control via Manipulation of Forebody Flow Asymmetrics
Forebody vortex control
Effect of Freestream Noise on Roughness-Induced Transition for the X-51A Forebody
A review of forebody vortex control scenarios
AERODYNAMIC FOREBODY SHAPE FOR VAN TRAILER
Wing rock generated by forebody vortices
Effect of a single strake on the forebody vortex asymmetry
1. Calculated values of the aerodynamical loads on a tangent-ogive forebody compare well -with experimental data.
计算出的空气动力数据与实验结果吻合。
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2. On the basis of the above, the mechanism is investigated by which the chine forebody can delay delta wing vortex burst.
在此基础上，对融合体前体延迟翼涡破裂的机理进行了深入探讨。
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3. The paper gives variations in the forebody drag, the normal force and the pressure center in accordance with the Mach Numbers and the geometric parameters.
给出了前阻、法向力及压心随马赫数或几何参数的变化曲线。
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4. This paper introduces a wind tunnel experimental method of projectile with jet from its forebody and influence of jet on aerodynamic characteristics of projectile.
介绍弹丸前体喷流实验方法及喷流对弹丸气动性能的影响。
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5. A study is carried out on a hypersonic inlet with rectangular-to-circular shape transition and forebody using numerical simulation and high enthalpy wind tunnel test.
对一种带前体的高超声速矩转圆形进气道开展了数值仿真及高焓脉冲风洞试验研究。
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6. When a fighter aircraft or missile flies at high angle of attack(AOA), asymmetric vortexes are produced from the forebody and induce strong side force and yawing moment.
飞机或导弹在大迎角下飞行时会形成非对称涡，从而产生很大的侧滑力和偏航力矩。
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7. The forebody, suspension lines and canopy were modeled as a series of elastically connected mass nodes. The flow field inside the canopy was two-dimensional inviscid, incompressible flow.
前体、伞绳及伞衣离散为一系列弹性连接的质量节点，伞衣内部流场为二维无粘、不可压流。
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8. 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。
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9. 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。
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forebody
