微型飞行器空气动力学研究

来源 :系统工程理论与实践 | 被引量 : 0次 | 上传用户：sunsand

【摘要】

：

围绕与微型飞行器相关的低雷诺数空气动力学问题,进行了低雷诺数翼型气动特性的数值分析研究、低马赫数低雷诺数流场数值计算方法研究、考虑扑翼结构弹性变形的气动特性估算

【作者】

：

李占科宋笔锋张亚锋

【机构】

：

西北工业大学航空学院,西北工业大学航空学院,西北工业大学航空学院陕西西安710072,陕西西安710072,陕西西安710072

【出处】

：

系统工程理论与实践

【发表日期】

：

2005年09期

【关键词】

：

微型飞行器雷诺数扑翼风洞试验

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论文部分内容阅读

围绕与微型飞行器相关的低雷诺数空气动力学问题,进行了低雷诺数翼型气动特性的数值分析研究、低马赫数低雷诺数流场数值计算方法研究、考虑扑翼结构弹性变形的气动特性估算方法研究、微型飞行器气动特性估算的非定常涡格法研究和微型飞行器的风洞试验研究,取得的研究成果对微型飞行器的发展具有重要的参考价值和指导意义.

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微型飞行器空气动力学研究

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