| 腹支撑对具有大展弦比机翼和船尾形机身的飞机模型的于扰与修正 |
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| 引用本文： | 崔乃明,张祥明,范召林.腹支撑对具有大展弦比机翼和船尾形机身的飞机模型的于扰与修正[J].实验流体力学,1994(1). |
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| 作者姓名： | 崔乃明 张祥明 范召林 |
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| 作者单位： | 中国空气动力研究与发展中心 |
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| 摘 要： | 一种适用于具有大展弦比机翼和船尾形机身的飞机模型的腹部支撑方式、腹支装置的设计要求和试验方法、以及腹支撑干扰的机理在此作了介绍，并给出了一些实验结果和对实验数据的修正方法．
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| 关 键 词： | 支架干扰，运输机，风洞试验技术 风洞数据修正 |
VENTRAL SUPPORT INTERFERENCE AND CORRECTION FOR AN AIRPLANE MODEL WITH HICH ASPECT RATIO WINGS AND BOATTAIL BODY |
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| Cul Naiming, Zhang Xiangming, Fan Zhoulin.VENTRAL SUPPORT INTERFERENCE AND CORRECTION FOR AN AIRPLANE MODEL WITH HICH ASPECT RATIO WINGS AND BOATTAIL BODY[J].Experiments and Measur in Fluid Mechanics,1994(1). |
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| Authors: | Cul Naiming Zhang Xiangming Fan Zhoulin |
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| Abstract: | A ventral support mode applicable to an airplane model with high aspect ratio wings and boattail body is presented in this paper. The requirement for ventral supporting design and the experimental method are outlined. The mechanism of ventral support interference with model is analyzed. Some test results and the method of correction to test data are also given. |
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| Keywords: | support interference transport wind tunnel data correction wind tunnel test technique |
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