Other
Scientific paper
Feb 2005
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..587p&link_type=abstract
Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,
Other
Scientific paper
The Plasma Wind Tunnel (PWT) SCIROCCO located at CIRA (Capua, Italy), is a hypersonic facility where the atmospheric conditions around the space vehicles during re-entry are reproduced. The Validation Phase of the SCIROCCO facility is at present on going. Here, it is important to investigate the flow uniformity at the nozzle exit by injecting transversal cold flow. Since it is very difficult to carry out this investigation in SCIROCCO, it has been developed in the Small Plasma Entry Simulator (SPES) at the University of Naples, because of its lower power and scale. In the present paper, the results obtained in the SPES facility about the mixing effects on the flow uniformity are shown and a comparison with the results obtained in the SCIROCCO facility during the development of a preliminary mixing test campaign.
de Filippis F.
Esposito Alfredo
Purpura C.
Renis R.
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