An extensive test campaign was performed in DLRs arc-heated facility L3K on a generic nosecap model. This model was specially designed to show influence of thermo-mechanical fluid-structure interaction when exposed to a high enthalpy flow. Tests were run at two flow conditions and different angles of attack. Due to orthotropic material properties the stagnation point heating caused a deformation, which could be measured by a displacement sensor. But also the aerodynamic pressure makes a substantial contribution to the fluid-structure interaction, which must not be neglected. The results of all temperature, pressure and displacement measurements will be gathered to build up an experimental database for the validation of coupled numerical sim...
Mastering aerothermal fluid-structure interaction (FSI) is crucial for theefficient and reliable des...
In the present study a numerical coupling tool for fluid-thermal structure interaction is validated ...
The purpose of the present investigation is the validation of a numerical coupling tool for fluid-th...
An extensive test campaign was performed in DLR's arc-heated facility L3K on a generic nosecap model...
An extensive test campaign was performed in DLR's arc-heated facility L3K on a generic nosecap model...
A generic nosecap model was tested in the arc heated facility L3K. The model was particularly design...
The thermo-mechanical behaviour of highly loaded components of space vehicles, as e.g. nosecaps and ...
Supersonic and hypersonic vehicles experience significant aerothermal loads from the exterior flowfi...
The focus of this degree thesis is the validation of a numerical environment for the coupled analysi...
Experiments have shown that a high-enthalpy flow field might lead under certain mechanical constrain...
Experimental tests have been carried out to analyze the effect of wall-to-total temperature ratio on...
The present investigation is aimed to evaluate the improvement of heat flux predictions for hyperson...
Reliable experimental data from ground and flight tests is critical for improving physical models an...
The arc heated wind tunnel LBK of DLR is used to investigate the response of heat protection materia...
The simple configuration is described and used for computational and experimental investigations inc...
Mastering aerothermal fluid-structure interaction (FSI) is crucial for theefficient and reliable des...
In the present study a numerical coupling tool for fluid-thermal structure interaction is validated ...
The purpose of the present investigation is the validation of a numerical coupling tool for fluid-th...
An extensive test campaign was performed in DLR's arc-heated facility L3K on a generic nosecap model...
An extensive test campaign was performed in DLR's arc-heated facility L3K on a generic nosecap model...
A generic nosecap model was tested in the arc heated facility L3K. The model was particularly design...
The thermo-mechanical behaviour of highly loaded components of space vehicles, as e.g. nosecaps and ...
Supersonic and hypersonic vehicles experience significant aerothermal loads from the exterior flowfi...
The focus of this degree thesis is the validation of a numerical environment for the coupled analysi...
Experiments have shown that a high-enthalpy flow field might lead under certain mechanical constrain...
Experimental tests have been carried out to analyze the effect of wall-to-total temperature ratio on...
The present investigation is aimed to evaluate the improvement of heat flux predictions for hyperson...
Reliable experimental data from ground and flight tests is critical for improving physical models an...
The arc heated wind tunnel LBK of DLR is used to investigate the response of heat protection materia...
The simple configuration is described and used for computational and experimental investigations inc...
Mastering aerothermal fluid-structure interaction (FSI) is crucial for theefficient and reliable des...
In the present study a numerical coupling tool for fluid-thermal structure interaction is validated ...
The purpose of the present investigation is the validation of a numerical coupling tool for fluid-th...