ramjet missile meaning in English
冲压式喷气发动机导弹
Examples
- A faster and better optimization of integrated design of integral rocket - ramjet missile with gacom
基于遗传算法的组合优化方法在整体式冲压发动机导弹一体化设计中的应用 - Integral rocket - ramjet is a propulsion system with great potential . using missile - engine integrated design method to realize the conceptual design of integral rocket - ramjet missile is of great significance to improve quality and efficiency of missile design
整体式火箭冲压发动机是一种很有前途的动力装置，采用导弹和发动机一体化设计方法进行整体冲压式导弹的总体设计，对于提高导弹的设计质量和设计效率具有重要的意义。 - According to the results , the performance of algorithms is assessed . since genetic algorithm has global searching ability and complex algorithm has capacity in searching local optimum , they are combined to optimize integrated ramjet missile design problem , and better result is gained
将这两种算法应用于整体式冲压发动机巡航导弹一体化设计实例中，评估算法的计算性能，并将遗传算法和复合形优化算法结合，对设计问题进行优化，得到了更好的优化结果。 - The key technology in integrated design of rocket - ramjet missile is discussed - - interference and restriction , also the method and framework of this integrated design are presented . based on each subsystem models , a computer aided integrated design system is set up for integral rocket - ramjet anti - ship missile
( 5 )对整体式冲压发动机导弹一体化设计的关键技术问题：发动机和导弹在一体化设计中的相互影响、相互制约关系进行了研究，提出了进行整体式冲压发动机导弹一体化设计的方法和框图。 - Collaborative optimization method is studied in depth , the causes leading to computational difficulty of this method are discussed by optimization theory and computation examples , and improve method which may solve this problem is presented . based on the comparison of several optimization methods and the characteristics of modern rocket - ramjet , step optimization pattern - a new integrated design mode is presented and is used to realize integrated design of rocket - ramjet . inner and outer fiowfield of a certain integral rocket - ramjet missile is simulated numerically using n - s equation
( 2 )系统地研究了导弹总体优化设计方法，探讨了多学科设计优化的原理、框架结构、具体表述形式，深入研究了协作优化方法的原理，从优化原理和算例两方面讨论了造成协作优化方法计算困难的原因，提出了可能克服这种计算困难的改进途径；在比较几种优化方法的基础上，针对新一代冲压式导弹的特点，提出了一体化设计的模式? ?分步优化模式，进行了整体式火箭冲压发动机反舰导弹总体参数的一体化设计。