A research program has been underway for four years to study vortex interaction aerodynamics that are relevant to military air vehicle performance. The program has been conducted under the auspices of the NATO Science and Technology Organization (STO), Applied Vehicle Technology (AVT) panel by a Task Group with the identification of AVT-316. The Missile Facet of this group has concentrated their work on the vortical flow field around a generic missile airframe and its prediction via computational methods. This paper focuses on mesh-related effects and RANS simulations. Simulated vortex characteristics were found to depend strongly on the properties of the employed mesh, in terms of both resolution and topology. Predictions of missile aerody...
This study focusses on the numerical simulation of supersonic flows around a missile with lattice wi...
A study of the aerodynamic characteristics of two missile configurations has been performed using th...
This study focuses on the numerical simulation of supersonic flows around a missile with lattice win...
A research program has been underway for four years to study vortex interaction aerodynamics that ar...
Vortex dominated flows provide a challenge for modern computational fluid dynamics (CFD) solvers to ...
This paper provides a brief overview of the activities undertaken by the Missile Facet of NATO STO A...
In this study, the influence of the turbulence model, grid resolution and flow solvers on the result...
Within the framework of the NATO Science and Technology Organization Applied Vehicle Technology Task...
Hybrid Reynolds Average Navier-Stokes (RANS) - Large Eddy Simulations (LES) have been applied to pre...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
Communication to : RTO AVT Symposium on vortex flow and high angle of attack, Loen (Norvege), May 07...
Subsonic flowfields over a missile configuration are computed at high angles of attack ranging from ...
The current investigations look at the vortical flow and aerodynamic performance of a generic sharp ...
This paper contains an investigation on the ability of some of the current turbulence models to pred...
Within the NATO Research and Technology Organisation Applied Vehicle Technology (AVT)-161 task group...
This study focusses on the numerical simulation of supersonic flows around a missile with lattice wi...
A study of the aerodynamic characteristics of two missile configurations has been performed using th...
This study focuses on the numerical simulation of supersonic flows around a missile with lattice win...
A research program has been underway for four years to study vortex interaction aerodynamics that ar...
Vortex dominated flows provide a challenge for modern computational fluid dynamics (CFD) solvers to ...
This paper provides a brief overview of the activities undertaken by the Missile Facet of NATO STO A...
In this study, the influence of the turbulence model, grid resolution and flow solvers on the result...
Within the framework of the NATO Science and Technology Organization Applied Vehicle Technology Task...
Hybrid Reynolds Average Navier-Stokes (RANS) - Large Eddy Simulations (LES) have been applied to pre...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
Communication to : RTO AVT Symposium on vortex flow and high angle of attack, Loen (Norvege), May 07...
Subsonic flowfields over a missile configuration are computed at high angles of attack ranging from ...
The current investigations look at the vortical flow and aerodynamic performance of a generic sharp ...
This paper contains an investigation on the ability of some of the current turbulence models to pred...
Within the NATO Research and Technology Organisation Applied Vehicle Technology (AVT)-161 task group...
This study focusses on the numerical simulation of supersonic flows around a missile with lattice wi...
A study of the aerodynamic characteristics of two missile configurations has been performed using th...
This study focuses on the numerical simulation of supersonic flows around a missile with lattice win...