Experimental tests in the arc wind tunnel in Naples (named SPES), aimed at stating the rarefaction level of the jet, were previously processed by a steady, one-dimensional and non-diffusive code. In this paper the same experimental data have been processed once again by more reliable codes like the Navier-Stokes (FLUENT) and the Direct Simulation Monte Carlo (DS2V) solvers, in order to consider the influence of the viscosity, the thermal conductivity and the diffusion of chemical species. The evaluation of the rarefaction level relies on the computation of a number of parameters and on the comparison of the measured drag coefficients with the ones reported in the published literature and the ones obtained reducing the drag computed by DS2V....
The objectives of the present Action Group AD/AG-48 of the ‘Group for Aeronautical Research and Tech...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...
The aim of the thesis is the study of some problems of hypersonic rarefied Aerodynamics. More specif...
Experimental tests in the arc wind tunnel in Naples (named SPES), aimed at stating the rarefaction l...
It is well know that, due to a very aggressive environment and to the rather high rarefaction level ...
The lift and drag coefficients for a slender re-entry configuration are measured in the near continu...
Measurements of the aerodynamic forces acting on a 70◦ semiangle cone have been made in the small ar...
To analyze the effectiveness of the thermal assessment test, the simulation method of the ground tes...
An important aspect to be taken into account in the design of a re-entry vehicle is the evaluation o...
Hypersonic research needs various experimental techniques in order to cover the requirements of diff...
The WIND code, a Reynolds-averaged Navier-Stokes solver used for a variety of aerospace flow simulat...
Mature numerical flow solvers based on continuum (Navier-Stokes) and gas-kinetic (Direct Simulatio...
Airflow over a flat plate at zero incidence is investigated as a function of the Reynolds number Re ...
The ability of the WIND Navier-Stokes code to predict the physics of multi-species gases is investig...
With a view to designing tests in the arc wind tunnel Small Planetary Entry Simulator (SPES) at the ...
The objectives of the present Action Group AD/AG-48 of the ‘Group for Aeronautical Research and Tech...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...
The aim of the thesis is the study of some problems of hypersonic rarefied Aerodynamics. More specif...
Experimental tests in the arc wind tunnel in Naples (named SPES), aimed at stating the rarefaction l...
It is well know that, due to a very aggressive environment and to the rather high rarefaction level ...
The lift and drag coefficients for a slender re-entry configuration are measured in the near continu...
Measurements of the aerodynamic forces acting on a 70◦ semiangle cone have been made in the small ar...
To analyze the effectiveness of the thermal assessment test, the simulation method of the ground tes...
An important aspect to be taken into account in the design of a re-entry vehicle is the evaluation o...
Hypersonic research needs various experimental techniques in order to cover the requirements of diff...
The WIND code, a Reynolds-averaged Navier-Stokes solver used for a variety of aerospace flow simulat...
Mature numerical flow solvers based on continuum (Navier-Stokes) and gas-kinetic (Direct Simulatio...
Airflow over a flat plate at zero incidence is investigated as a function of the Reynolds number Re ...
The ability of the WIND Navier-Stokes code to predict the physics of multi-species gases is investig...
With a view to designing tests in the arc wind tunnel Small Planetary Entry Simulator (SPES) at the ...
The objectives of the present Action Group AD/AG-48 of the ‘Group for Aeronautical Research and Tech...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...
The aim of the thesis is the study of some problems of hypersonic rarefied Aerodynamics. More specif...