Fighter kites are usually small, flattened diamond-shaped ones made of paper and bamboo.
斗风筝用的通常是用纸和竹子做的小而平的菱形风筝。
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。
In this paper aimed at the application problem of certain aviation bomb for a certain fighter, a coincidental calculation method of bomb ballistic coefficient is proposed.
针对某型战机上挂载使用某型航空炸弹的问题，提出了一种炸弹弹道系数的符合计算方法。
This paper presents a. preliminary research on the feedback of feel of longitudinal mechanical control system connected with steering-engine in supersonic fighter.
本文对高空超音速飞机中与增稳舵机交联的纵向机械操纵系统的力反传问题作了理论探讨。
This paper discuss the requirements for pilot' s associate system as an equipment of future fighter of Air Force, also presents function partitioning, hardware configuration an…
本文讨论新一代战斗机对驾驶员辅助系统的需要，提出了它的功能划分、硬件配置和实时智能软件的设计要求与方法。
The longitudinal and lateral directional control effectiveness requirements of high maneuver aircraft are discussed in this paper, and the fighter J-7 is taken as an example.
本文讨论了高机动性飞机滚转机动飞行对纵横航向操纵效能的要求，并以J-7飞机为算例进行了验证。
The concept of fighter torsional agility and its metrics are introduced in this paper.
介绍了战斗机扭转敏捷性概念及其尺度。
This paper has analyzed and calculated the influence of external ZC-1 scout equipment on the lift coefficient, damp coefficient and aerodynamic center of the fighter plane.
从外挂对载机气动特性影响的计算方法出发，分析了现役某型战机外挂ZC-1航空侦察吊舱对载机升力系数、阻力系数和气动中心的影响，得出了具体的计算结果。
After contrasting with some fighter plane in existence, the method discussed in this paper is feasible and can be used for tactic-technology requirement analysis.
经过实际型号的验算，证明本文提出的算法，精度较高，方法可行。
This paper discuss the requirements for pilot' s associate system as an equipment of future fighter of Air Force, also presents function partitioning, hardware configuration and the design methods …
本文讨论新一代战斗机对驾驶员辅助系统的需要，提出了它的功能划分、硬件配置和实时智能软件的设计要求与方法。
In this paper a relaxed static stability (RSS) fighter F16 is taken as an example to discuss deep stall corridor characteristics.
以放宽静稳定性（RSS）战斗机F-16为例，讨论了深失速走廊特性。 利用具有非线性气动力的简化运动方程，分析了飞机深失速特性；
In this paper, the transmission shaft of the all-moving horizontal tail for a fighter plane is considered as a structural system, and its failure probability is analysed.
本文从整个构件系统着眼，研究某型歼击机全动平尾转轴梁静强度的可靠性。
In this paper, the transmission shaft of the all-moving horizontal tail for a fighter plane is considered as a structural system, and its failure probability is analysed.
本文从整个构件系统着眼，研究某型歼击机全动平尾转轴梁静强度的可靠性。
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