Finally, an engineering approach for nearly shock-free wing design is introduced.
最后介绍了近无激波机翼修型的工程设计方法。
In order to validate the philosophy and software of supercritical wing design, a training plane is refitted and its high lift system is redesigned.
为进行超临界机翼气动设计技术的飞行验证，将某教练机改装为飞行验证机，为此必须进行增升装置的重新设计。
Composite wing design, in which involved are many disciplines such as structural mechanics, aerodynamics and control engineering, is a complicated process.
复合材料翼面设计是一个涉及结构力学、空气动力学和控制工程等多个学科的复杂过程。
Collaborative Optimization based on approximate technology is applied to plane wing design.
将本文研究的基于近似技术的协同优化方法应用在机翼设计中。
The main problems include general design of towed system, controllable wing design and intergration of optical sensors.
着重解决的问题包括拖曳系统的总体设计、控制翼的设计以及光学类传感器的集成。
Based on model design and rotary wing design of helicopters, this paper introduces a multi targets inverse eigenvalue problem and gives a parallel method.
由模型设计和直升机旋翼设计问题出发，归纳出一类多目标逆特征值问题并提出一种适合在并行计算机上实现的并行算法。
Based on model design and rotary wing design of helicopters, this paper introduces a multi targets inverse eigenvalue problem and gives a parallel method.
由模型设计和直升机旋翼设计问题出发，归纳出一类多目标逆特征值问题并提出一种适合在并行计算机上实现的并行算法。
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