Micro balloon actuator array for aerodynamic control of delta wing has been explored in this paper.
本文就以用于三角翼气动控制的微气泡致动器阵列为对象展开研究。
The design is fuzzy control aerodynamic control transmission system in the clean production of a typical programme.
该设计是模糊控制控制气动传动系统在清洁生产方面的一个典型方案。
This paper integrates direct lateral force control with aerodynamic control, taking the anti-aircraft missile which has the anti-guided ability in the aerosphere as research subject.
本文的研究对象为大气层内具有反导能力的防空导弹。主要研究内容为把直接侧向力控制与气动力控制结合。
The key components of the system consist of a tail section with aerodynamic control surfaces, a (body) strake kit, and a combined inertial guidance system and GPS guidance control unit.
该系统的主要组件，包括一个具有表面空气动力控制的尾段，一个(身体)稳流边条套件，以及组合惯性导引系统和GPS全球定位导引控制基件。
Building more aerodynamic aircraft and operating them more efficiently (by reducing air-traffic-control delays, for instance) could produce about two-thirds of those savings.
制造更符合空气动力学的飞机，并用更有效的方式来运营飞机——例如减少空中交通控制而产生的延误，这些方法可以为这些节省做出大约三分之二的贡献。
We do not yet know how to achieve the desired control during the aerodynamic phase of flight.
我们只是还不知道怎么在航行的空气动力学方面，对飞机实现需要的控制。
Because their two sets of wings effectively flap as one, that in theory gives them little control over the aerodynamic forces on their body.
因为它们的两副翅膀叠在一起，在空气动力学的理论中，这意味着它们对自己身体缺乏控制力。
Flight control was performed by gas jets and aerodynamic surfaces.
飞行控制由燃气喷口和气动面实现。
The flight control of airplane with a precise model under an uncertain information condition of aerodynamic parameters, is a typical example.
具有准确模型的飞机在不准确气动参数信息条件下的飞行控制就是一个典型例子。
To execute online warning and active control for aerodynamic instability of compressors, aerodynamic instability inception must be detected accurately and timely.
要对压气机气动失稳进行在线预警和主动控制，就必须能够准确、及时地检测到失稳先兆。
An aerodynamic optimization method is described which is based on dynamic boundary control. This method is according to the idea of controlling the boundary of transforming object.
本文根据控制变形物体边界变化的思想，建立了一种基于动态边界控制的气动优化设计方法。
Control measures for wind-induced vibration have mainly aerodynamic measures, structural measures and mechanical measures.
风致振动控制的措施主要有气动措施、结构措施和机械措施三种。
On military aircraft, hydraulic pressures of actuators caused by hinge torque vary with aerodynamic force on control surface due to different flight states.
飞机在不同的飞行阶段和飞行状态下，由于作用在控制面上的气动负载不同，因而由铰链力矩引起的液压作动筒压力也在变化。
Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences.
空气动力元件以及具有空气动力元件的机翼，伺服驱动-控制模块，计算机，计算机程序和用于影响尾迹涡流的方法。
In addition, a number of control parameters are selected to study their impact on aerodynamic efficiency and pneumatic power.
此外，还选取若干个控制参数，研究其对气动效率和气动功率的影响。
Based on the mechanical and aerodynamic methods of shock wave control, a method of plasma aerodynamic actuation is proposed.
在机械式和气动式激波控制方法的基础上，提出了激波控制的等离子体气动激励方法。
Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle.
为了优化无人驾驶航空飞行器在整个飞行过程中的空气动力特性而使机身、推进系统和升力控制面一体化的设计技术。
The leading edge vortices are important factor to control the flow field around the slender-wing and to influence the aerodynamic characteristics of the wing.
细长翼翼面上方的前缘集中涡是控制机翼绕流和影响机翼气动力特性的主要因素。
According to the demand of flight control system, a nonlinear dynamics model with considerable aerodynamic forces and moments for a large maneuver re entry missile head is built.
根据飞行控制要求，考虑了影响较大的气动力和气动力矩因素，建立了一个完全表征大机动情况下弹头运动的非线性动力学模型。
An idea for the aerodynamic design of a strake-wing is proposed from the control standpoint with utilization of vortex and separated flows.
本文从控制和利用旋涡分离流的观点出发，说明了边条机翼的设计思想。
To the kinetic interceptor with lateral impulse thrust and aerodynamic force, it is required to solve the problem of combined fire of motors for attitude control.
针对具有侧向脉冲推力和气动力复合控制的动能拦截弹，需要解决姿控发动机的组合点火问题。
The aerodynamic forces on any control surface produce a moment about the hinge.
在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
In a modern aircraft, for example, the power boost controls amplify the force applied by the pilot to move the control surface against large aerodynamic forces.
例如在现代飞行器中，动力助推控制系统将飞行员的力放大以推动受到很大的气流作用的机翼表面。
The aerodynamic forces on the tail boom have been calculated and their changes with the circulation control variables were drawn in curves.
根据测量数据计算出尾梁上气动力随环量控制参数的变化情况，并绘制成曲线。
Based on the 3d aerodynamic stability model, the related active control technique and the open-loop transfer function have been provided, in which the three dimensional flow effects are involved.
在轴流压气机三维气动稳定性模型的基础上，给出了考虑轴流压气机三维效应的主动控制模型及其传递函数。
Along with the deep development of study, the microjet technology will be possibly applied to control the aerodynamic flow of the high speed aircraft surface and the thrust vector of rocket engine.
并指出，随着研究工作的深入，该项技术还可望用于高马赫数飞行体表面气体流动控制、火箭发动机推力方向控制等。
The aerodynamic terms in the force and moment equations have all been replaced by the state variables of which they are functions. and control forces and moments.
力和力矩方程中的空气动力项已经全部用为其函数的状态变量及操纵力和力矩所代替。
A numerical method is presented for predicting unsteady transonic aerodynamic flow about aircraft wings with control surface.
本文介绍一种带操纵面机翼的非定常跨声速流的有限差分计算方法。
The aerodynamic characteristics of the free wing are investigated in this paper. The wind tunnel test results shows that the control of the angle of attack of the fre…
通过风洞试验，对带升降副翼控制的自由翼气动特性也进行了实验研究，验证了位于自由翼后缘的升降副翼可有效地控制自由翼相对气流的平衡迎角。
The aerodynamic characteristics of the free wing are investigated in this paper. The wind tunnel test results shows that the control of the angle of attack of the fre…
通过风洞试验，对带升降副翼控制的自由翼气动特性也进行了实验研究，验证了位于自由翼后缘的升降副翼可有效地控制自由翼相对气流的平衡迎角。
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