Add to ORKGConsidered is the computation problem of turbulent flow past aircraft configuration, and configuration components, for Mach numbers up to transonic and hypersonic values. Discussed are the problem of transition laminar-turbulent, and especially the choice, application and validation of turbulence models ranging from scalar models to transport-equation models of all kind. Special attention is given to separated flow, where the still insufficient predictions make new ways of treatment necessary, first of all, however, a sound diagnosis where and why current statistical turbulence models fail. (orig.)SIGLEAvailable from TIB Hannover: RR 2803(538) / FIZ - Fachinformationszzentrum Karlsruhe / TIB - Technische InformationsbibliothekDEGerman
A brief review is given of turbulence models in use today for engineering applications. The main cat...
This work aims at providing numerical methods that enable the robust and efficient simulation of tur...
A turbulence model based on a synthetic eddy method (SEM) has been adapted for flight simulation pur...
The paper considers one of the stages of atmospheric entry for aerospace craft. The aim is to invest...
IntroductionTurbulence generally plays a key role in drag generation, heat transfer, particle disper...
For aerodynamic performance prediction of aircraft or aircraft components in the industrial design p...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
One- and two-equation turbulencemodels are examined for hypersonic perfect- and real-gas owswith la...
Accurate prediction of turbulent flows remains a challenging task despite considerable work in this ...
At the present time, aerodynamic analysis and numerical methods are inexorably linked. Thus, a quali...
This paper reports on the development of a unified one-equation model for the prediction of transiti...
The computational fluid dynamics (CFD) tools for various flow problems have become widespread nowada...
This paper reports on the development of a unified one-equation model for the prediction of transiti...
Four turbulence models are described and evaluated for transonic flows over the High-Speed Research/...
SIGLEAvailable from British Library Document Supply Centre-DSC:9113.125(96/06) / BLDSC - British Lib...
A brief review is given of turbulence models in use today for engineering applications. The main cat...
This work aims at providing numerical methods that enable the robust and efficient simulation of tur...
A turbulence model based on a synthetic eddy method (SEM) has been adapted for flight simulation pur...
The paper considers one of the stages of atmospheric entry for aerospace craft. The aim is to invest...
IntroductionTurbulence generally plays a key role in drag generation, heat transfer, particle disper...
For aerodynamic performance prediction of aircraft or aircraft components in the industrial design p...
Aeronautical aerodynamics is characterized by compressible flow at high Reynolds numbers. Therefore ...
One- and two-equation turbulencemodels are examined for hypersonic perfect- and real-gas owswith la...
Accurate prediction of turbulent flows remains a challenging task despite considerable work in this ...
At the present time, aerodynamic analysis and numerical methods are inexorably linked. Thus, a quali...
This paper reports on the development of a unified one-equation model for the prediction of transiti...
The computational fluid dynamics (CFD) tools for various flow problems have become widespread nowada...
This paper reports on the development of a unified one-equation model for the prediction of transiti...
Four turbulence models are described and evaluated for transonic flows over the High-Speed Research/...
SIGLEAvailable from British Library Document Supply Centre-DSC:9113.125(96/06) / BLDSC - British Lib...
A brief review is given of turbulence models in use today for engineering applications. The main cat...
This work aims at providing numerical methods that enable the robust and efficient simulation of tur...
A turbulence model based on a synthetic eddy method (SEM) has been adapted for flight simulation pur...