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Shock Tunnel Operation and Correlation of Boundary Layer Transition on a Cone in Hypervelocity Flow

机译:震动隧道运行与边界层过渡在超细流中锥体上的相关性

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We have re-examined the correlation of transition onset data with tunnel operating conditions by modeling transition onset location with two-dimensional response surfaces in terms of h_(res) and P_(res) variables. We observe a positive correlation of X_(tr) with h_(res) in both air and N_2 and a negative correlation of X_(tr) with P_(res). The parameter Re_(tr)~* exhibits a positive correlation with reservoir pressure in both gases. Controlling for variations in P_(res), no statistically significant dependence of Re~(tr)~* on h_(res) was found for either the present air or N_2 data or the historical air data in Adam and Hornung. We explore an alternative normalization of the transition onset location by the local laminar boundary layer thickness X_(tr)/δ_(.99) and find that this is essentially independent of the edge Mach number for a given gas type and pressure range (Figure 5). We examine the correlation of transition onset with the most amplified acoustic frequency in the boundary layer and find that lower frequencies correlate with smaller values of normalized transition distance X_(tr)/δ_(.99), suggesting that the frequency-dependent amplification of the tunnel noise may be responsible for the observed systematic variations in transition onset distance.
机译:我们通过在H_(RES)和P_(RES)变量方面,通过使用二维响应表面建模转换开始位置来重新检查转换发作数据与隧道操作条件的相关性。我们观察到空气和N_2中的H_(RE)与H_(RE)的正相关和具有P_(RE)的X_(TR)的负相关性。参数RE_(TR)〜*表现出与两种气体中的储层压力的正相关。控制P_(RES)的变化,没有发现RE〜(TR)〜*对H_(RES)的统计学上显着的依赖性,用于ADAM和Hornung中的目前的空气或N_2数据或历史空中数据。我们通过局部层状边界层厚度X_(TR)/Δ_(。99)探索过渡开始位置的替代归一化位置,并发现这基本上与给定的气体类型和压力范围的边缘MACH编号无关(图5 )。我们研究了边界层中最放大的声学频率的转换发作的相关性,并发现较低频率与较小的归一化转换距离X_(TR)/Δ_(。99)相关联,表明频率依赖性放大隧道噪声可能负责观察到的过渡开始距离的系统变化。

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