平板翼型动态失速下的气动性能研究
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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共引文献10
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