Despite the sensitivities of turbulence intensities, the agreement for the mean and friction velocities between PIV, Pitot and numerical predictions are promising, so that the

(2006) measured turbulent spots progressing on a blunt cylindrical body with spherical nose in hypersonic flow (Mach 8.9 free stream; Mach 3.74 at the edge of the boundary layer)

Wall Contour Coordinates after Boundary Layer Correction and Mach Number Distribution for the Subsonic Two-dimensional Nozzle.. Wall Contour Coordinates after

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

The relationship of the freestream external disturbance field environment to the boundary layer disturbances that are ultimately responsible for transition are significant to

and Monson, D.J., “The Hypersonic Shock Wave- Turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2,” AIAA Paper No. and Shapey, B.L.,

Visual features input to the implemented ESA EO Level 2 SCM classifier are: MS color names detected by the Satellite Image Automatic Mapper  (SIAM  ) lightweight computer

It was found that the coating having 2D cavities of aspect ratio 0.3 and porosity 0.8 triggers the new instability whose growth rate can be larger than that of Mack second mode..

The study shows that the selected eddy-viscosity turbulence models, in combination with a constant Prandtl number model for turbulent heat flux, give good predictions of the

Computations are performed for hypersonic flow at a free stream Mach number of 6.0 over a 5-degree half-angle cone with blunt leading edge, R n =0.001 in, for different

In this study, we found that ES936 (NQO1 inhibitor) and NQO1 siRNA could enhance TRAIL-induced apoptosis in endometrial carcinoma Ishikawa cells, demonstrating that the effect

monitored the rms of the freestream flow field throughout the calibration process... The completed calibration matrix included a CVA output voltage corresponding to each

Figure 14: Heat flux ratios determined by Baldwin and Lomax and k − ω turbulence models in proposed two-shock model with second cone base radius of 13. 28 which was not observed in

Those two flight projects are the Hypersonic Boundary layer Transition (HyBoLT) flight experiment and the Shuttle Boundary Layer Transition Flight Experiment (BLT

Figure 7 Histopathological effects of ACA and CDDP treatment on HSC-4 human oral squamous carcinoma xenograft tumor biopsies against members of the NF- κ B pathway and NF- κ B

Lower wall temperature reduces the sound speed within the boundary layer (increasing the local Mach number), so it is perhaps unsurprising that the reduced wall temperature has

In this thesis an analysis of the weakly nonlinear stability of viscous (Mack’s first mode) disturbances in the hypersonic boundary layer on a sharp slender cone with passive

Another key equation in the study of the physics of turbulence is the Reynolds stress tensor transport equation, the formulation of which was described earlier. The