Feasibility of particle image velocimetry for low-speed unconventional vapor flows

Journal Article (2019)
Author(s)

Adam Joseph Head (TU Delft - Flight Performance and Propulsion)

P Colonna (TU Delft - Flight Performance and Propulsion)

F. Schrijer (TU Delft - Aerodynamics)

M. Gallo (Hogeschool Inholland, TU Delft - Flight Performance and Propulsion)

Matteo Novara (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

Research Group
Flight Performance and Propulsion
Copyright
© 2019 A.J. Head, Piero Colonna, F.F.J. Schrijer, M. Gallo, M. Novara
DOI related publication
https://doi.org/10.1016/j.expthermflusci.2018.10.028
More Info
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Publication Year
2019
Language
English
Copyright
© 2019 A.J. Head, Piero Colonna, F.F.J. Schrijer, M. Gallo, M. Novara
Research Group
Flight Performance and Propulsion
Volume number
102
Pages (from-to)
589-594
Reuse Rights

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Abstract

This work assesses the feasibility of the planar PIV technique to study the characteristics of a siloxane vapor D4. Titanium dioxide (TiO2) seeding particles were used to track the motion around a rotating disk in a low speed flow. Vector fields of natural convection (NC) and a superposition of NC and rotating flow were selected as exemplary cases. The particles were capable of tracing the flow since the calculated Stokes number St is 6.5×10-5. The quality of the experimental data is assessed by means of particle seeding density and particle image Signal to Noise ratio (S/N). The final results are deemed acceptable for an accurate assessment of the flow field. Rejected outliers are below 2.3% and the relative uncertainties corresponding to the average velocity fields are below 1%.