The airflow around a helicopter and especially around the main rotor is very complex, non-uniform and highly non-linear. The wake of a helicopter’s main rotor interacts very strongly with the rotor itself, giving rise to a number of problems that can only be addressed if the geometry and intensity of the wake is known with a high degree of accuracy. The best compromise between computational cost and accuracy are vortex-lattice formulations known as Freewake codes. The Institute of Flight Systems of the German Aerospace Center (DLR) in cooperation with DLR’s Simulation and Software Technology operates a modern Freewake implementation which has been optimized for computations on a workstation using GPGPU accelerators. The code is coupled via ...
AbstractA full-span free-wake method is coupled with an unsteady panel method to accurately predict ...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
In contrast to an aircraft’s propeller the wake of a helicopter’s main rotor interacts very strongly...
OpenACC allows offloading calculations to accelerators such as GPGPUs using short compiler directive...
In flow simulations of helicopter configurations the blade-vortex-interactions have a significant in...
Free-vortex wake models are capable of providing an accurate and physically detailed representation ...
Helicopters operating from ships are exposed to turbulent airwakes which can determine ship-helicopt...
This paper presents a feasibility study for trimming the computational fluid dynamics model of a com...
The Freewake code from the DLR Institute of Flight Systems simulates the 3d flow around a rotor of a...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
The miss-distance between helicopter rotor blades and their tip vortices is a key parameter for the ...
A loosely coupled simulation is presented for a helicopter rotor in forward flight. The aeromechanic...
The problem of helicopter rotor wake aerodynamics during maneuvering flight conditions was analyzed ...
This dissertation describes the implementation and validation of a coupled rotor-fuselage simulation...
AbstractA full-span free-wake method is coupled with an unsteady panel method to accurately predict ...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
In contrast to an aircraft’s propeller the wake of a helicopter’s main rotor interacts very strongly...
OpenACC allows offloading calculations to accelerators such as GPGPUs using short compiler directive...
In flow simulations of helicopter configurations the blade-vortex-interactions have a significant in...
Free-vortex wake models are capable of providing an accurate and physically detailed representation ...
Helicopters operating from ships are exposed to turbulent airwakes which can determine ship-helicopt...
This paper presents a feasibility study for trimming the computational fluid dynamics model of a com...
The Freewake code from the DLR Institute of Flight Systems simulates the 3d flow around a rotor of a...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
The miss-distance between helicopter rotor blades and their tip vortices is a key parameter for the ...
A loosely coupled simulation is presented for a helicopter rotor in forward flight. The aeromechanic...
The problem of helicopter rotor wake aerodynamics during maneuvering flight conditions was analyzed ...
This dissertation describes the implementation and validation of a coupled rotor-fuselage simulation...
AbstractA full-span free-wake method is coupled with an unsteady panel method to accurately predict ...
This dissertation describes three aspects of the comprehensive rotorcraft analysis. First, a physics...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...