Study of crossflow topology of unsteady vortex motion over a delta wing 三角翼非定常旋涡运动横截面拓扑结构研究
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Law of vortex motion 涡动定律
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The increase in heat transfer coefficients and the concomitant pressure drops inserts is found to be strongly influenced by tape - induced vortex motion and higher flow velocity due to the tube blockage . 4mpa 。试验系统地研究了在该re数范围空气流动的传热和流阻特性，获得了不同压力、温度，不同扭转比下的数据。
