The present study is the logical continuation of a former paper by the first author in which the influence of the chemical models by Gupta and by Park on the computation of heat flux on the Orion and EXPERT capsules was evaluated. Tests were carried out by the direct simulation Monte Carlo code DS2V and by the computational fluid-dynamic (CFD) code H3NS. DS2V implements the Gupta model, H3NS implements the Park model. In order to compare the effects of the chemical models, the Park model was implemented also in DS2V. The results showed that DS2V and H3NS compute a different composition both in the flow field and on the surface, even using the same chemical model (Park). Furthermore DS2V computes, by the two chemical models, different compos...
Aeroheating predictions play an important role in the heatshield design of Mars entry capsule. This ...
A hypersonic vehicle crosses many regimes, from rarefied to continuum, as the vehicle descends throu...
Future exploration programs, promoted by the main world space agencies, deal with sample return miss...
The present study is the logical continuation of a former paper by the first author in which the inf...
The computation of heat flux on two current re-entry capsules, European eXPErimental Reentry Testbed...
This study is an extension of former works by the present authors, in which the influence of the che...
Four different chemical models (Bird, Fan and Shen, ‘classic’, and ‘new’ quantic) have been impleme...
The present work is the logical continuation of a paper by Zuppardi and Romano where the models by B...
The aim of the thesis is the study of some problems of hypersonic rarefied Aerodynamics. More specif...
A simplified model for the analysis of molecular and reaction dynamics in hypersonic flows of rarefi...
The aerodynamic behavior of the EXPERT capsule has been already widely studied at low altitudes. In ...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
The analysis of the risk from re-entry objects has become an important topic. Concerning the uncerta...
Several numerical analyses have been conducted to examine the effects of some state-of-the-art chemi...
Aeroheating predictions play an important role in the heatshield design of Mars entry capsule. This ...
A hypersonic vehicle crosses many regimes, from rarefied to continuum, as the vehicle descends throu...
Future exploration programs, promoted by the main world space agencies, deal with sample return miss...
The present study is the logical continuation of a former paper by the first author in which the inf...
The computation of heat flux on two current re-entry capsules, European eXPErimental Reentry Testbed...
This study is an extension of former works by the present authors, in which the influence of the che...
Four different chemical models (Bird, Fan and Shen, ‘classic’, and ‘new’ quantic) have been impleme...
The present work is the logical continuation of a paper by Zuppardi and Romano where the models by B...
The aim of the thesis is the study of some problems of hypersonic rarefied Aerodynamics. More specif...
A simplified model for the analysis of molecular and reaction dynamics in hypersonic flows of rarefi...
The aerodynamic behavior of the EXPERT capsule has been already widely studied at low altitudes. In ...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
The analysis of the risk from re-entry objects has become an important topic. Concerning the uncerta...
Several numerical analyses have been conducted to examine the effects of some state-of-the-art chemi...
Aeroheating predictions play an important role in the heatshield design of Mars entry capsule. This ...
A hypersonic vehicle crosses many regimes, from rarefied to continuum, as the vehicle descends throu...
Future exploration programs, promoted by the main world space agencies, deal with sample return miss...