18 results with keyword: 'three dimensional shock wave boundary layer interactions'
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
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Figure 1.7 Power spectra of unsteady pressure loading beneath a compression ramp SBLI 12 Figure 1.8 Wall pressure time-series beneath intermittent region of separation shock
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In 3D SWTBLI, a free shear layer with strong mean shear strength and low kinetic energy is generated when flow is detached near the mean separation line.. The free shear layer
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(2002) looked at relatively low-frequency correlations in the same compression-corner flow and found significant correlations between upstream velocity fluctuations and the
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The effects of lambda-shock formations which indicate possible boundary layer separations, reflections of shock waves, and shock wave – boundary layer interactions on inlet
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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
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( 2006 )): (i) the undisturbed flow upstream of the SWBLI where the Stanton number distribution is unaffected by the shock impingement; (ii) a zone with significantly reduced
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3.66 Reynolds stress profiles for the lagRST-1 model showing grid convergence downstream of the separation
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It may thus be supposed that the origin of low-frequency unsteadiness in the turbulent regime is also associated with the nonlinear interaction between instability modes arising in
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The boundary layer state at the shock impingement location was varied from laminar to turbulent to investigate the heat flux amplification in transitional SWBLI for three
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Figure 3. Microtubule-associated proteins 2 and neurofila- ments increased in the primary somatosensory cortex during the first month of life. Arrowheads show dendritic and
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The purpose of this letter is to document the traffic and parking impacts associated with the construction of a liquor store at the existing Fort Myers Beach Publix
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Figure 6(a) portrays relatively large streamwise fluctuations within the incoming boundary layer that are energetically associated with a broad spanwise region of fluctuations
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boundaries of the outlet plane, the upper surface and the lateral surface 2 as shown in Figure 1(b) are treated with the non-reflective boundary condition [45,46]. To reduce
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The scalability of the interactions induced by impinging shock waves traveling over the turbulent boundary layer with nearly constant shock strengths has been experimen- tally
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