Chinese translation for "ramjet missile"
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- 冲压式喷气发动机导弹
Related Translations:
ramjet: 冲压发动机冲压喷气发动机冲压喷射冲压式喷气发动机冲压喷气式喷气机喷射推理引擎之一种
- Example Sentences:
| 1. | 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 | | 2. | 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。 | | 3. | 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。 | | 4. | 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。 | | 5. | 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。 | | 6. | This design system can be applied to mdo because of its modular structure . aerodynamic characteristics , propulsion system and integrated design aspects related to integral rocket - ramjet missile are studied thoroughly in this paper , which has important reference value and instructional significance in the development of integral rocket - ramjet missile
本文对整体式冲压发动机导弹涉及的有关气动、动力与机弹一体化设计方面的问题进行了比较全面深入的研究，对我国整体式冲压发动机导弹的研制具有重要的参考价值与指导意义。 | | 7. | Also longitudinal aerodynamic characteristics of missile are investigated . the traditional dependence on wind tunnel experiment is changed greatly : firstly , the aerodynamic characteristics of missiles with complex configuration are solved satisfactorily , especially integral rocket - ramjet missile ; secondly , feasibility of n - s equation to numerical simulation of inner and outer fiowfield of missile with complex configuration is discussed
( 3 )采用n - s方程方法数值模拟某型整体式冲压发动机导弹的全弹内外流场，研究了导弹的纵向气动特性，改变了过去依赖于地面风洞试验结果的传统做法。 |
- Similar Words：
- "ramjet exhaust nozzle" Chinese translation, "ramjet helicopter" Chinese translation, "ramjet ignition system" Chinese translation, "ramjet inlet" Chinese translation, "ramjet interior" Chinese translation, "ramjet nacelle" Chinese translation, "ramjet operating limits" Chinese translation, "ramjet performance" Chinese translation, "ramjet propulsion" Chinese translation, "ramjet propulsion testing" Chinese translation
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