0000000000263533

AUTHOR

F. De Filippis

showing 3 related works from this author

Comparison between probe stagnation point heat flux measurements and correlation formulas in SCIROCCO plasma wind tunnel tests

2012

A large part of the SCIROCCO Arc Heater Performance Map has been investigated. The heat flux measurements at the stagnation point of t he facility Calibratio Probe have been used to find an experimental fit. Such a formula ha s been compared with the predictions of the De Filippis-Serpico equation and the well known Fay-Riddell formula. Finally the experimental fit has been also compared with the Sa gner-Verant formula obtained at the ONERA F4 hypersonic plasma wind tunnel.

Arc (geometry)Hypersonic speedClassical mechanicsHeat fluxmeasurements scirocco plasma wind tunnel testsPhysics::Space PhysicsSettore ING-IND/06 - FluidodinamicaPlasmaMechanicsStagnation pointMathematicsWind tunnel
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Experimental Characterisation of the CIRA Plasma W...

2005

Materials scienceAnalytical chemistryPlasma56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law
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Experimental characterisation of the CIRA plasma wind tunnel SCIROCCO test section

2008

Abstract During the Validation Phase of the CIRA-PWT SCIROCCO Facility located at Capua (Italy), a test campaign has been carried out to verify the performances of the facility with the use of the two conical nozzle configurations “D” and “F” with exit diameters are, respectively of, 1150 and 1950 mm. For the first time the data results of the tests have been used to characterize the plasma flow in the test section of the facility. In particular, analytical relationships between the main thermo-fluid-dynamic parameters in the test section and the reservoir conditions of the facility have been found, and compared to the CFD prediction developed during the Design Phase of the facility. Very i…

EngineeringBoundary layerbusiness.industrySection (archaeology)NozzleAerospace EngineeringStructural engineeringConical surfaceComputational fluid dynamicsbusinessBoundary layer thicknessDisplacement (fluid)Wind tunnelActa Astronautica
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