Development of Efficient Methods for Aerodynamic Design of Aircrafts
Sebastian Arvidson, Saab Aerosystems/Chalmers
Shia-Hui Peng, FOI/Chalmers
Per Weinerfelt, Saab Aerosystems
|Sponsors:||Vinnova, Saab Aerosystems|
|Start of project:||September 2009|
|End of project:||May 2017|
Today, the traditional way to work with aerodynamic design in aircraft industry is challenged by tougher requirements on shorter through put times, cost effectiveness and rise in product quality. CFD is a very important tool in aircraft design, thus it has to be improved to align with these requirements.
The flow fields analyzed in aircraft industry are often complex. Speed ranges typically from subsonic to supersonic. A wide range of spatial scales as well as time scales are used. Parts of the flow can be highly viscous and turbulent while other parts, more or less, can be inviscous. The need for highly resolved boundary layers and secondary flows in combination with complex geometries gives meshes with a large number of calculation points. Therefore, it is important that the calculation methods are robust and time efficient.
In aircraft design today, the most common way to analyze viscous flows is to use RANS. This, however, implies limitations in many parts of the aircraft envelope, since most of the flows are unsteady and time dependent. For example flight conditions at high angles of attack, buffeting effects over a wing or separation from inlet lips due to aircraft maneuvering.
In order to increase the possibility to efficiently simulate unsteady flows around the aircraft with high
accuracy, this project will focus on improving today´s methodology and calculation methods, i.e.
improving turbulence modeling, mainly hybrid RANS-LES methods, and numerical algorithms as well as
improve the methodology for running and evaluate time dependent CFD-calculations in an industrial environment.
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