| 一种带前缘襟翼或缝翼的机翼的跨声速试验 |
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| 引用本文： | 龚卫斌.一种带前缘襟翼或缝翼的机翼的跨声速试验[J].实验流体力学,1989(4). |
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| 作者姓名： | 龚卫斌 |
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| 作者单位： | 北京空气动力研究所 |
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| 摘 要： | 本文叙述了一种典型的带前缘襟翼或缝翼的切尖三角机翼,在跨超声速风洞中,进行跨声速测压、测力试验研究的情况。给出部分带有前缘襟翼的机翼压力分布曲线及有副翼偏角的测力试验曲线。从机翼压力分布的积分与测力试验结果看到,两者很接近,其结果均符合线性理论及跨声速波动规律。
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| 关 键 词： | 跨声速特性 机翼 压力分布 |
TRANSONIC TEST FOR A WING WITH LEADING EDGE FIAP OR SLAT |
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| Gong Weibin.TRANSONIC TEST FOR A WING WITH LEADING EDGE FIAP OR SLAT[J].Experiments and Measur in Fluid Mechanics,1989(4). |
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| Authors: | Gong Weibin |
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| Institution: | Beijing lnstitute of Aerodynamics |
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| Abstract: | The paper presents a tran-Sonic test research for a modernwing in the transonic and Supersonic wind tunnel and presents the meas-ured aerodynamic characteristics of pressures and forces.The wing in-cludes the leading edge flap,leading edge slats and aileron.The force meas-urement data agree with that from the integral of the measured pressuredistribution. |
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| Keywords: | transonic characteristics wing pressure distribution |
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