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Effects of homogeneous condensation in compressible flows: Ludwieg-tube experiments and simulations

Published online by Cambridge University Press:  23 January 2007

XISHENG LUO ,
GRAZIA LAMANNA ,
A. P. C. HOLTEN  and
M. E. H. VAN DONGEN
XISHENG LUO
Affiliation:
Department of Applied Physics, Eindhoven University of Technology, Eindhoven, The Netherlands
GRAZIA LAMANNA
Affiliation:
Institute of Aerospace Thermodynamics, Universität Stuttgart, Stuttgart, Germany
A. P. C. HOLTEN
Affiliation:
Department of Applied Physics, Eindhoven University of Technology, Eindhoven, The Netherlands
M. E. H. VAN DONGEN
Affiliation:
Department of Applied Physics, Eindhoven University of Technology, Eindhoven, The Netherlands
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Abstract

Effects of homogeneous nucleation and subsequent droplet growth in compressible flows in humid nitrogen are investigated numerically and experimentally. A Ludwieg tube is employed to produce expansion flows. Corresponding to different configurations, three types of experiment are carried out in such a tube. First, the phase transition in a strong unsteady expansion wave is investigated to demonstrate the mutual interaction between the unsteady flow and the condensation process and also the formation of condensation-induced shock waves. The role of condensation-induced shocks in the gradual transition from a frozen initial structure to an equilibrium structure is explained. Second, the condensing flow in a slender supersonic nozzle G2 is considered. Particular attention is given to condensation-induced oscillations and to the transition from symmetrical mode-1 oscillations to asymmetrical mode-2 oscillations in a starting nozzle flow, as first observed by Adam & Schnerr. The transition is also found numerically, but the amplitude, frequency and transition time are not yet well predicted. Third, a sharp-edged obstacle is placed in the tube to generate a starting vortex. Condensation in the vortex is found. Owing to the release of latent heat of condensation, an increase in the pressure and temperature in the vortex core is observed. Condensation-induced shock waves are found, for a sufficiently high initial saturation ratio, which interact with the starting vortex, resulting in a very complex flow. As time proceeds, a subsonic or transonic free jet is formed downstream of the sharp-edged obstacle, which becomes oscillatory for a relatively high main-flow velocity and for a sufficiently high humidity.

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Papers
Information
Journal of Fluid Mechanics , Volume 572 , February 2007 , pp. 339 - 366
Copyright
Copyright © Cambridge University Press 2007

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