The present numerical investigation of the cold spray process examines the gas and
particle dynamics both inside and outside the nozzle in the context of improving particle
deposition. In the first part of the investigation, the one-dimensional isentropic relations
coupled with the drag force acting on a particle is employed in a parametric study of
the nozzle performance. Next, the addition of a barrel section to the end of the nozzle
is proposed and shown to be more efficient in some cases than using the diverging
section of the nozzle for particle acceleration. Finally, the effect of nozzle wall friction
is incorporated to assess the amount of deviation from the isentropic model.
The gas and particle dynamics between the nozzle and substrate during the steady
cold spray process is the focus of the second part of the investigation. An underexpanded
and overexpanded nozzle is employed to accelerate the particles and the operating
conditions were set to those used in the validation cases. The particle impact statistics
are extracted to provide information on the particle impact speed, angle and location.
The particles are also tracked during their flight between the nozzle and substrate to
characterise their response to changes in the gas flow. It was found that the variation in
particle speed across the embedded shock structures became minimal as the diameter
increased. For particles with a Stokes number greater than one, the nozzle exit velocity
may be used as an approximation of the impact speed. A theoretical model is also
proposed for calculating the particle impact speed using the nozzle exit conditions.
The deployment of the shock tube in cold spray is a recent innovation in which a
planar shock is released into the ambient air towards a substrate while the particles
are injected across the wake of the shock. Although the process suffers from a number
of practical limitations, monodisperse particles are used to compare the impact speed
produced by steady and unsteady cold spray processes. It was found that this process
also offers a mean of studying the shock formation process in underexpanded impinging
jets. The shock speeds were selected such that either a shock diamond or Mach disk
is reproduced in the impingement region characteristic of a moderately and highly
underexpanded jet. Although the unsteady cold spray process requires a much lower
driving pressure to produce the impact speeds found during the steady process, there
are several practical limitations associated with it.