This paper presents an approach to possibility of direct force control on the joined wing configuration.
对连接翼气动布局实现直接力控制的可能性进行了初步的探索。
Finally, it is suggested that the flying wing configuration is an optimal selection of aerodynamic configuration design of an UCAV for reconnaissance.
最后，指出飞翼布局是无人侦察作战飞机气动布局的较好选择。
In order to study the wing rock characteristics of a fighter, the wing rock characteristics for a fighter with delta wing configuration is investigated in this paper.
为了研究战斗机的机翼摇滚特性，运用风洞试验和数值模拟手段，对一典型三角翼布局开展了研究工作。
The joined-wing configuration, as compared with the normal configuration, is characterized by low structural weight, small induced drag, big lift coefficient and good stability.
联结翼布局与常规布局相比具有结构重量轻、诱导阻力小、升力系数大和稳定性良好的特点。
The team used simulation tools to show it was possible to achieve over-land flight by dramatically lowering the level of sonic booms through the use of an "inverted-V" engine-under wing configuration.
这个团队在其所设计的飞机模型中在引擎上方使用了一个“倒V字型”的结构，他们通过模拟工具展示了通过这个结构可戏剧性地减少音爆导致的噪声成为一种可能。
Numerical results show that present method is an effective one for solving the flow around wing body configuration with control surface deflection.
数值算例表明本文方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Internal fuel fraction may also be high, given the fuselage configuration and large internal volume of the big delta wing.
内部油箱可能也很大，考虑到机身的尺寸和起巨大的三角翼的内部空间。
Two types of lay-ups of the composite wing, namely, circumferentially uniform stiffness (CUS) configuration and circumferentially asymmetric stiffness (CAS) configuration, are investigated.
研究了机翼的两种铺设方式：即周向均匀刚度配置（CUS）和周向反对称刚度配置（CAS）。
The viscous flow around M6 wing and F4 wing-body configuration are simulated and compared with the results of wind tunnel experiment.
为了验证方法和程序的正确性，论文中对M6机翼和F4翼身组合体的流场进行了数值模拟，并与试验结果进行了对比。
The paper investigates the problem on vortex generator control boundary layer's separation of supercritical airfoil and wing for body configuration wing.
本文研究涡流发生器控制超临界翼型和翼身组合体机翼的附面层分离问题。
According to the computing results, the relations between the he stability characteristics and the configuration parameters of joined-wing airplanes were obtained.
然后应用中心复合试验设计法确定了七十种外形布局，并计算和分析了各外形参数变化对联结翼飞机稳定性的影响。
The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
从全速位方程出发研究了机翼和翼身融合体跨音速绕流的有限元算法。
On the basis of the canard configuration a contour stealthy design including chiefly the wing, the fuselage and their connection type is projected.
在鸭式布局的基础上，对飞行器各部件及部件间的连接方式进行了外形隐身设计。
The results show that joined-wing layout with a flat concealed body have great potentialities for the configuration.
结果显示，具有扁平机身的连接翼方案是一个有潜力的无人机布局形式。
The wing vortex breakdown on canard on configuration was delayed relative to that on canard off configuration, but the canard vortex broke down very early.
鸭式布局主翼涡破裂较无鸭翼布局有所延迟，但鸭翼自身涡系破裂较早。
Early autogyros resembled the fixed-wing aircraft of the day, with wings and a front-mounted engine and propeller in a tractor configuration to pull the aircraft through the air.
早期自转旋翼机有着与固定翼航空器类似的机翼和前置的动力装置，拖动自身向前飞行。
The aircraft is adopted with the swept forward wing is not a new configuration, but the unmanned aircraft is adopted with the swept forward wing is unprecedented.
飞机采用前掠翼气动布局并非鲜为人知，但无人驾驶飞机采用前掠翼却前所未有。
About multi - control surface configuration with elevators, its dynamic model was established under pitch movement, differing from wing with ailerons alone.
针对此翼面上有升降舵的多舵面布局，建立了俯仰运动下不同于翼面上只有副翼的动力学模型。
This article investigates the flow control technique of forward-swept wing blended body (FBB) tailless configuration by means of wind tunnel tests.
通过风洞试验研究了前掠翼融合体无尾气动布局(FBB布局)的流动控制技术。
The saucer-shaped aircraft is a novel aircraft adopting blend-wing-body configuration.
碟形飞行器是一种新颖的，采用翼身融合布局的飞行器。
The saucer-shaped aircraft is a novel aircraft adopting blend-wing-body configuration.
碟形飞行器是一种新颖的，采用翼身融合布局的飞行器。
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