Add to ORKGNumerical simulations of shock-shock interactions in front of a circular cylinder have been performed. The numerical results of a validation test case are compared with experimental data. The modelling of a perfect gas and a mixture of chemically reacting perfect gases have been applied to reentry flow conditions. Differences of the results of the two models are demonstrated in view to the calculated shock configurations and the peak loads on the surfac
As part of the studies, at the Aerothermodynamics and Hypersonics Division (EAH) of the Institute fo...
The research uses CFD to investigate the internal flow of two hypersonic engine inlets: the Hyperson...
The problem of shock-shock interaction between a planar oblique shock wave and a bow shock wave is u...
Results of an ongoing validation project for hypersonic flow prediction, which involves both numeric...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The interaction of shock waves is investigated for a two-dimensional model flow and compared with ex...
The shock-shock interaction in front of a cylinders is investigated numerically to identify the peak...
Numerical simulations are carried out in the non-continuum flow regime to analyze flow features in t...
This project presents a computational study of hypersonic reentry flow over a blunt body. Fluent™ co...
Results of numerical simulations of Mach 10 air flow over a hollow cylinder-flare and a double-cone ...
Possibilities to manipulate shock/boundary layer interactions are demonstrated with regard to an app...
The best approach for conducting the research necessary for developing hypersonic flight vehicles is...
The flowfield analysis around a model of re-entry capsule has been carried out utilizing the Finite ...
The temperature in the front region of a hypersonic vehicle nose can be extremely high, for example,...
A computational methodology has been developed to investigate the transient start of a Reaction Cont...
As part of the studies, at the Aerothermodynamics and Hypersonics Division (EAH) of the Institute fo...
The research uses CFD to investigate the internal flow of two hypersonic engine inlets: the Hyperson...
The problem of shock-shock interaction between a planar oblique shock wave and a bow shock wave is u...
Results of an ongoing validation project for hypersonic flow prediction, which involves both numeric...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The interaction of shock waves is investigated for a two-dimensional model flow and compared with ex...
The shock-shock interaction in front of a cylinders is investigated numerically to identify the peak...
Numerical simulations are carried out in the non-continuum flow regime to analyze flow features in t...
This project presents a computational study of hypersonic reentry flow over a blunt body. Fluent™ co...
Results of numerical simulations of Mach 10 air flow over a hollow cylinder-flare and a double-cone ...
Possibilities to manipulate shock/boundary layer interactions are demonstrated with regard to an app...
The best approach for conducting the research necessary for developing hypersonic flight vehicles is...
The flowfield analysis around a model of re-entry capsule has been carried out utilizing the Finite ...
The temperature in the front region of a hypersonic vehicle nose can be extremely high, for example,...
A computational methodology has been developed to investigate the transient start of a Reaction Cont...
As part of the studies, at the Aerothermodynamics and Hypersonics Division (EAH) of the Institute fo...
The research uses CFD to investigate the internal flow of two hypersonic engine inlets: the Hyperson...
The problem of shock-shock interaction between a planar oblique shock wave and a bow shock wave is u...