Simulations performed with variable wall temperature confirmed the scaling analysis, and we conclude that if the objective is to reduce the flow separation, cooling must be applied in

The effects of lambda-shock formations which indicate possible boundary layer separations, reflections of shock waves, and shock wave – boundary layer interactions on inlet

It can be noticed that the SST k- ω turbulence model predicts the roughness effects on shock boundary layer interaction flows more reasonably compared to the wall

SVA Model uses the set of algorithms (1) Graphed-based Structure Algorithm (Social Network Analysis: SNA) to analyze the key factors of influencing nodes about

Table 1 presents the comparison of performance metrics between baseline and the optimized geometry (B6032). The optimized geometry shows higher pressure recovery and

As an ICC employee, you are eligible to participate in either the Iowa Public Employees’ Retirement System (IPERS) or in the Iowa Association of Community College Trustees’

samples, color indices were to be correlated with government grade, sell-.. ing

To identify the shock movement, distortion and unsteadiness during the processes of the supersonic starting jet impingement and shock wave boundary layer interaction

The line load test on the handrail is applied at a height of 1.1m. For typical balustrade installations line loadings of 1.5 kN/m, infill panel UDL loads of 1.5 kN/m 2 , and

(2002) looked at relatively low-frequency correlations in the same compression-corner flow and found significant correlations between upstream velocity fluctuations and the

Chamberlain, Rachel P., "Articulations of Liberation and Agency in Yanagi Miwa's "Elevator Girls"." Thesis, Georgia State University,

Figure 6.47 shows that the typical Mach reflection configuration found in the inviscid simulation (shown in Figure 6.49) does not occur when the viscous effects are accounted

The asymptotic behavior of shock wave – boundary layer interactions is investigated for cases of strong interaction between the laminar boundary layer and attached leading edge

The introduction of streaks in a supersonic boundary layer, in which the transition onset is driven by oblique first-mode instabilities, is expected to have a destabilizing

Of interest is how these wall models perform in comparison to a Wall-Resolved Large Eddy Simulation (WR-LES) and experimental results of a shock turbulent boundary layer

Although still greater than the baseline, for increasing lateral spacing the boundary layer thickness along the plane of symmetry of the SBVG pair reduces. The increase of

as SBLI (shock wave boundary layer interaction) in the scientific literature. The interaction of shock waves on wall boundary layer has always been an active area of interest due to

Методами флуоресцентної спектроскопії, флуоресцентної кореляційної спектроскопії та ЛКС було знайдено, що каліксарени 23–26 утворюють міцелярні наночастинки розміром від 3