| 高超声速巡航飞行器气动布局优化软件设计 |
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| 引用本文： | 江志国,唐硕,车竞.高超声速巡航飞行器气动布局优化软件设计[J].飞行力学,2008,26(1):52-55. |
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| 作者姓名： | 江志国 唐硕 车竞 |
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| 作者单位： | 西北工业大学,航天学院,陕西,西安,710072 |
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| 摘 要： | 从总体性能指标角度出发,采用面向对象的编程方法,基于Visual C 开发了高超声速巡航飞行器气动布局优化软件。整个优化软件分为参数化建模模块、面元生成模块、性能指标计算模块、优化算法模块。各模块之间相对独立,通过函数接口实现互联,具有非常好的可维护性、可重用性和可扩展性。该软件实现了对高超声速巡航飞行器的气动力、气动热、隐身性能、操稳性能等总体性能指标进行气动布局多目标的优化,能够满足高超声速巡航飞行器概念研究和初步设计要求。
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| 关 键 词： | 高超声速巡航飞行器 优化设计 优化软件 算法 |
| 文章编号： | 1002-0853（2008）01-0052-04 |
| 收稿时间： | 2007-01-24 |
| 修稿时间： | 2007-07-20 |
Integrated Optimization Design for a Hypersonic Cruise Vehicle |
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| JIANG Zhi-guo,TANG Shuo,CHE Jing.Integrated Optimization Design for a Hypersonic Cruise Vehicle[J].Flight Dynamics,2008,26(1):52-55. |
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| Authors: | JIANG Zhi-guo TANG Shuo CHE Jing |
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| Abstract: | Based on system performance,guided by an object-oriented method,an integrated optimization design system of a hypersonic cruise vehicle was built through VC .The system realization multi-objective integrated optimization design for the hypersonic cruise vehicle,includes modules of parameter-modeling,surface element-build,performance-calculation and optimize-arithmetic.Each module interlinks via interface of function.The integrated optimization performance includes aerodynamics forces,aerodynamics heating,stealth performance,control and stability.The object-oriented method made this system have better maintainability,high reusability and better expansibility.This system has been successfully applied to concept research and principium design of the hypersonic cruise vehicle. |
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| Keywords: | hypersonic cruise vehicle optimization design optimization software algorithm |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
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