Numerical study of shock-turbulent boundary layer interactions with incipient and complete separation
This paper aims at describing the main features of a separated boundary layer in shock reflection at a Mach number of 2.3. The data used for this analysis were taken from large eddy simulations of the interactions for three-shock intensities, resulting in flow cases from incipient to fully separated. Computational results were validated versus expe...
Effect of various leachate recirculation strategies on batch anaerobic digestion of solid substrates
Published in International Journal of Applied Pattern Recognition
An empirical study of researchers' and practitioners' views on compensating major highway project contractors