H. K. Versteeg

*Introduction. *Conservation Laws of Fluid Motion and Boundary Conditions. *Turbulence and its Modelling. *The Finite Volume Method for Diffusion Problems. *The Finite Volume Method for Convection-Diffusion Problems. *Solution Algorithms for Pressure-Velocity Coupling in Steady Flows. *Solution of Discretised Equations. *The Finite Volume Method for Unsteady Flows. *Implementation of Boundary Conditions. *Advanced topics and applications. Appendices. References. Index.

This paper reviews the past research, experimental techniques and scaling relationships used in the studies of oscillatory buoyant diffusion flames and reports an experimental investigation conducted to determine the pulsating characteristics of such flames. The experimental data were obtained by using three techniques, namely, pressure fluctuation measurements, thermal imaging and high-speed video photography. Present findings are compared with data sets reported in the literature and correlations for pulsation frequency suggested by previous studies are independently verified. Analysis of the experimental data on frequency of pulsations in different burners shows that for a fixed-diameter flame the pulsation frequency is almost independent of fuel flow rate. The equation f=1.68D−0.5 gives the best approximation for the relationship between pulsating frequency and diameter over a wide range of data. An alternative way of expressing the relationship between the key variables is St=0.52*(1/Fr)0.505. This proves to be a better way of expressing the relationship since it can include the effect of the fuel flow rate. Slight modifications to this expression allows prediction of flame oscillations under elevated/reduced gravity and isothermal buoyant plumes. This relationship and the observations of the present study confirm the hydrodynamic nature of flame puffing: interplay of buoyancy and fluid motion. © 1996 by John Wiley & Sons, Ltd.

Aerosol delivery of plasmid DNA therapeutic solutions is promising for the treatment of respiratory diseases. However, it poses challenges, most significantly the need to protect the delicate supercoiled (sc) structure of plasmid during aerosolization. Nebulizers for liquid aerosolization using meshes appear a better method for delivery than conventional jet and ultrasonic nebulizers. This paper explores their application to the delivery of plasmid DNA. A computational fluid dynamics model of the dynamics of fluid flow through the nozzle of the MicroAIR mesh nebulizer indicated high strain rates (>10(5) s(-1)) near the nozzle exit capable of causing damage to the shear-sensitive plasmid DNA. Knowledge of the strain rates predicted using CFD and molecule size determined using atomic force microscopy (AFM) enabled estimation of the hydrodynamic force and whether damage of shear-sensitive therapeutics was likely. Plasmids of size 5.7 and 20 kb were aerosolized in the mesh nebulizer. The sc structure of the 5.7-kb plasmid was successfully delivered without damage, while aerosolization of the 20-kb plasmid led to disintegration of the pDNA sc structure as observed in AFM. Subsequent formulation of the sc 20-kb plasmid with PEI resulted in successful aerosol delivery. The maximum hydrodynamic forces computed for the aerosolization of structures of the size of 5.7-kb and PEI formulated 20-kb plasmids were less than the forces reported to damage the structure of double-stranded DNA. A combination of CFD analysis and structure analysis may be used to predict successful aerosol delivery in such a mesh nebulizer.