Title :
Measurement technology of the impact of alumina liquid particles on a hot surface
fDate :
6/21/1905 12:00:00 AM
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;
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on
Conference_Location :
Toulouse
Print_ISBN :
0-7803-5715-9
DOI :
10.1109/ICIASF.1999.827151