DocumentCode
1689498
Title
Measurement technology of the impact of alumina liquid particles on a hot surface
Author
Fauchais, P.
fYear
1999
fDate
6/21/1905 12:00:00 AM
Firstpage
42705
Lastpage
42712
Abstract
The aim of this study, carried out in the frame of the ASSM (Aerodynamics of Segmented Solid Motors) research program, is a better understanding of the phenomena that govern the interactions between liquid alumina particles and a hot surface or liquid alumina film. To achieve it, a complex experimental device has been designed and built. In a controlled argon atmosphere chamber are set two plasma torches and a reclining substrate. This set-up allows the use of carbon-carbon substrates. The first plasma torch produces molten alumina particles, and the second one heats the substrate up to 2300 K. An optical diagnostic characterizes the in-flight parameters of a single particle : its size and velocity by PDA (Particle Doppler Anemometry) and its temperature by two-color fast (100 ns) pyrometry. An imaging technique monitors the impact mode: splashing, deposition or rebound. For the latter the rebounding angle and velocity can be measured. A laser beam is used for visualization of trajectories in a narrow wavelength band-pass. For each droplet, its size, velocity and temperature are measured and impact is observed. The goal is to investigate how the impact mode is influenced by these parameters
Keywords
aerospace propulsion; aluminium; drops; flow visualisation; high-temperature techniques; impact (mechanical); particle size measurement; plasma torches; pyrometers; velocity measurement; 100 ns; 2300 K; Al; Ar; Particle Doppler Anemometry; alumina liquid particles; argon atmosphere chamber; carbon-carbon substrates; deposition; droplet; hot surface; liquid alumina film; optical diagnostic; plasma torches; rebound; rebounding angle; reclining substrate; size measurement; splashing; temperature measurement; two-color fast pyrometry; velocity measurement; visualization of trajectories; Aerodynamics; Particle measurements; Plasma devices; Plasma diagnostics; Plasma temperature; Solids; Substrates; Temperature measurement; Velocity measurement; Wavelength measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on
Conference_Location
Toulouse
Print_ISBN
0-7803-5715-9
Type
conf
DOI
10.1109/ICIASF.1999.827151
Filename
827151
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