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平板翼型动态失速下的气动性能研究

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摘要 本文基于SST k-w模型对平板翼型的动态失速问题展开数值模拟研究,以翼型的1/2弦长处为转动中心,分析翼型在不同俯仰角速度下的气动性能,探究动态失速对平板翼型气动性能的影响。
出处 《黑龙江科技信息》 2015年第14期47-,共1页 Heilongjiang Science and Technology Information
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