可压缩湍流边界层摩擦阻力分解理论研究

来源 :第十届全国流体力学学术会议 | 被引量 : 0次 | 上传用户:liongliong478
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  阻力是空气动力学最重要的气动力参数之一,湍流摩擦阻力的分解与预测是学术界普遍关心的热点问题.目前,湍流摩擦阻力分解方法多局限于不可压缩流动,例如FIK和EZD方法,而对于可压缩湍流边界层的摩擦阻力分解方法尚不完善.本文基于流向时均动能方程,提出了可压缩湍流边界层摩擦阻力分解理论,对光滑和复杂可压缩壁湍流摩擦阻力分解进行了严格的推导,并从物理角度讨论了摩擦阻力产生的机制.为评估可压缩性对湍流摩擦阻力的贡献,开展了超声速槽道流的直接数值模拟,马赫数M=1.5,3,雷诺数Reτ=215,450,850,利用可压缩湍流摩擦阻力分解理论,研究了可压缩性贡献随马赫数和雷诺数变化的变化趋势.研究结果表明流体可压缩性导致的附加分子粘性耗散贡献随马赫数增大而增大,随雷诺数增大而减小,本文进一步对粘性耗散和湍动能生成在槽道内的分布进行分析,物理地解释了边界层内湍流运动对摩擦阻力的影响.
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