All Outputs (6)

Multi-block high-order dns code development for jet in turbulent cross-flow simulation (2012)
Journal Article
Castagna, J., & Yao, Y. (2012). Multi-block high-order dns code development for jet in turbulent cross-flow simulation. Journal of Algorithms and Computational Technology, 6(4), 593-621. https://doi.org/10.1260/1748-3018.6.4.593

A multi-block high-order finite-difference direct numerical simulation (DNS) code has been developed for studying turbulent flows over complex geometries. A global mapping technique is adopted and applied to a multi-block domain arrangement, in which... Read More about Multi-block high-order dns code development for jet in turbulent cross-flow simulation.

Numerical study of unsteady airflow phenomena in a ventilated room (2012)
Journal Article
Horikiri, K., Yao, Y., & Yao, J. (2012). Numerical study of unsteady airflow phenomena in a ventilated room. Computational Thermal Sciences, 4(4), 317-333. https://doi.org/10.1615/ComputThermalScien.2012005093

Numerical simulation of airflow in an indoor environment has been carried out for forced, natural, and mixed convection modes, respectively, by using the computational fluid dynamics (CFD) approach of solving the Reynolds-averaged Navier-Stokes equat... Read More about Numerical study of unsteady airflow phenomena in a ventilated room.

CFD prediction and experimental measurement of blade water coverage in a diesel turbocharger (2012)
Journal Article
Yao, J., & Yao, Y. (2012). CFD prediction and experimental measurement of blade water coverage in a diesel turbocharger. Modelling and Simulation in Engineering, 2012, 1-11. https://doi.org/10.1155/2012/789563

A turbocharger unit for diesel engine is often equipped with a built-in online water washing system and its performance is not always satisfactory because of efficiency declination due to deposit accumulated on blade surfaces not being washed away. I... Read More about CFD prediction and experimental measurement of blade water coverage in a diesel turbocharger.

Effect of jet inclination angle and hole exit shape on vortical flow structures in low-reynolds number jet in cross-flow (2012)
Journal Article
Yao, Y., Maidi, M., & Yao, J. (2012). Effect of jet inclination angle and hole exit shape on vortical flow structures in low-reynolds number jet in cross-flow. Modelling and Simulation in Engineering, 2012, 1-7. https://doi.org/10.1155/2012/632040

Numerical studies have been performed to visualize vortical flow structures emerged from jet cross-flow interactions. A single square jet issuing perpendicularly into a cross-flow was simulated first, followed by two additional scenarios, that is, in... Read More about Effect of jet inclination angle and hole exit shape on vortical flow structures in low-reynolds number jet in cross-flow.

Flow topology and secondary separation modelling at crossing shock wave/turbulent boundary layer interaction conditions (2012)
Journal Article
Salin, A., Yao, Y., & Zheltovodov, A. (2012). Flow topology and secondary separation modelling at crossing shock wave/turbulent boundary layer interaction conditions. International Journal of Aerospace Innovations, 4(1-2), 13-28. https://doi.org/10.1260/1757-2258.4.1-2.13

Steady RANS modelling has been carried out for a symmetrical double-sharp-fin configuration with an inclination angle 15°, Mach 3.92 and Reynolds number Reδ = 3.08 x 105. Grid refinement and turbulence model influences using ω-based Reynolds Stress m... Read More about Flow topology and secondary separation modelling at crossing shock wave/turbulent boundary layer interaction conditions.

Shock induced separating flows in scramjet intakes (2012)
Journal Article
Yao, Y., Zheng, Y., & Rincon, D. (2012). Shock induced separating flows in scramjet intakes. International Journal of Modern Physics: Conference Series, 19(73), https://doi.org/10.1142/S2010194512008604

Shock induced separating flows in a scramjet intake has been studied by using a computational fluid dynamics approach. A configuration of scramjet intake geometry consisting of two exterior compression ramps, followed by a subsequent inlet and interi... Read More about Shock induced separating flows in scramjet intakes.