Titlebook: Whither Turbulence and Big Data in the 21st Century?; Andrew Pollard,Luciano Castillo,Mark Glauser Book 2017 Springer International Publis

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A 50-Year Retrospective and the FutureProfessor Owen Phillips. The goal was to examine how internal waves generated at a region of sharp density gradient were affected by an adverse current. As the waves steepened they broke into turbulence, then propagated in a different mode. A rather elegant theory could explain the steepening and wh

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Towards the Direct Numerical Simulation of a Self-similar Adverse Pressure Gradient Turbulent Boundaessure gradient TBL (ZPG-TBL) developing on a flat surface from the same mean inflow conditions using the TBL direct numerical simulation (DNS) code of Simens et al. (J Comput Phys 228:4128–4231, 2009) and Borrell et al. (Comput Fluids 80:37–43, 2013). The APG-TBL DNS uses a modified wall-normal far

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Analysis of Velocity Structures in a Transitionally Rough Turbulent Boundary Layer friction. This effect is in particular felt in the roughness sub-layer (3. − 5., where . denotes the characteristic roughness height) and may extend across the boundary layer for .∕. < 50 as mentioned in [9] (note that . represents the boundary layer thickness). Knowledge of the effects of roughnes

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Streamwise Relaxation of a Shock Perturbed Turbulent Boundary Layere vast amounts of data. This is particularly true of high speed wall-bounded flows with embedded shocks which characterize many of today’s aerodynamic propulsion systems. As an example of the depth of analysis now attainable with the extensive databases available from the simulations, both mean and

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The Sound-Field Produced by Clustered Rockets During Start-Up ratios encompassing free-shock separated flow, restricted shock separated flow, and the end-effects-regime. The rocket plume is visualized using a retroreflective shadowgraphy system while an experimentally validated RANS model provides insight into the internal flow and shock structure patterns. P

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Variable Viscosity Jets: Entrainment and Mixing Processon between Constant Viscosity Flows and Variable Viscosity Flows, in a round jet, on the basis of the same initial conditions (same jet momentum and/or the same initial Reynolds number). The two fluids are density-matched. A propane jet issues into a slight nitrogen coflow for which the kinematic vi

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