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首页> 外文会议>Proceedings of the 3rd Sino-Italian conference on space aerothermodynamics and hot structures >Distributions of Heat Flux on Leading Edges of Wings with Some Deflection Angle
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Distributions of Heat Flux on Leading Edges of Wings with Some Deflection Angle

机译：具有一定偏转角的机翼前缘的热通量分布

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摘要

For the wing with some deflection angle, the upwind angle and the deflection angle will directly influence the position where heat flux is the highest. In this paper, the function equation about the upwind angle and the deflection angle and the deviation angle (Deviate the center line on the lending) was derived based on the triangle knowledge of the ball surface. When the any two angles were determined among the three angles discussed above, another angle was also obtained according to the equation, which was the place where the heat flux was the highest. The result would well agree with the experimental results and the empirical results, which almost satisfies engineering requirements.
机译：对于具有一定偏转角的机翼，迎风角和偏转角将直接影响热通量最大的位置。本文基于球面的三角形知识，导出了迎风角，偏转角和偏离角的函数方程（偏离借出中心线）。当在上述三个角度中确定任意两个角度时，还根据等式获得另一个角度，这是热通量最高的地方。结果与实验结果和经验结果吻合良好，几乎可以满足工程要求。

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