0000000000173050

AUTHOR

P. Barrera

showing 5 related works from this author

GROUP ANALYSIS AND SOME EXACT SOLUTIONS FOR THE THERMAL BOUNDARY LAYER

2006

We perform the group analysis of the thermal boundary layer in laminar flow. We obtain the classification of the solutions in terms of the asymptotic velocity. Some solutions of the boundary layer equations, for some distributions of outer flow velocity, are obtained also.

LayerBurger's equationThermalBoundarySettore ING-IND/06 - Fluidodinamicasolitary waveSolitons
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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 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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Painlevé analysis and exact solutions for the coupled Burgers system

2006

We perform the Painleve test to a system of two coupled Burgers-type equations which fails to satisfy the Painleve test. In order to obtain a class of solutions, we use a slightly modified version of the test. These solutions are expressed in terms of the Airy functions. We also give the travelling wave solutions, expressed in terms of the trigonometric and hyperbolic functions.

Class (set theory)Nonlinear Sciences::Exactly Solvable and Integrable SystemsAiry functionHyperbolic functionMathematics::Classical Analysis and ODEsTraveling waveApplied mathematicsOrder (group theory)TrigonometryPainlevé Burgers-type equationsMathematicsWIT Transactions on Engineering Sciences, Vol 52
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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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