Add to ORKGThis paper presents a utter analysis for the supercritical CAST 10-2 airfoil and the laminar NACA 64-008 airfoil in a flow with free boundary layer transition based on CFD computations. For transition prediction the γ-Re_θ transition model is used. The results are compared to fully turbulent results obtained with the SST k-ѡ model. Unsteady RANS computations at Re = 2e6� are used to determine the aerodynamic derivatives, required to identify the utter boundary for a 2 degree-of-freedom model. At the limits of the laminar drag bucket a decrease in utter stability can be found for both airfoils and the given structural model. However, the limits of the laminar bucket are strongly in uenced by the prescribed turbulence boundary conditions. I...
The flutter behavior of a supercritical airfoil is investigated using a panel formulation, which sol...
The steady flow aerodynamics of a cascade of compressor airfoils is computed using a two-dimensional...
Angle of attack has impact on transonic flow filed and aerodynamic force, but most of current resear...
This paper presents a flutter analysis for the supercritical CAST 10-2 airfoil in a flow with free b...
A laminar wing has a high potential in terms of fuel savings. It should however not lead to a reduct...
This paper presents a flutter analysis for a supercritical airfoil with free boundary layer transit...
Today a lot of attention is paid to the development of environmental friendly technologies. In the a...
Nowadays drag reductions are important also in aircraft design. Natural laminar flow on aircraft win...
This report presents results for CFD computations for 2d airfoil flows with free boundary layer tran...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
This paper introduces a local, correlation-based transition model used for CFD- based flutter predi...
In this paper a stability analysis of a laminar airfoil is presented and compared to turbulent flow ...
In this paper a stability analysis of a two dimensional laminar airfoil with two degrees-of-freedom ...
First results of a flutter experiment in transonic flow are presented. A wind tunnel model with the ...
A laminar wing test case for the flutter behavior in transonic flow with free boundary layer transit...
The flutter behavior of a supercritical airfoil is investigated using a panel formulation, which sol...
The steady flow aerodynamics of a cascade of compressor airfoils is computed using a two-dimensional...
Angle of attack has impact on transonic flow filed and aerodynamic force, but most of current resear...
This paper presents a flutter analysis for the supercritical CAST 10-2 airfoil in a flow with free b...
A laminar wing has a high potential in terms of fuel savings. It should however not lead to a reduct...
This paper presents a flutter analysis for a supercritical airfoil with free boundary layer transit...
Today a lot of attention is paid to the development of environmental friendly technologies. In the a...
Nowadays drag reductions are important also in aircraft design. Natural laminar flow on aircraft win...
This report presents results for CFD computations for 2d airfoil flows with free boundary layer tran...
A Navier-Stokes Computational Fluid Dynamics (CFD) code is coupled with a Computa-tional Structural ...
This paper introduces a local, correlation-based transition model used for CFD- based flutter predi...
In this paper a stability analysis of a laminar airfoil is presented and compared to turbulent flow ...
In this paper a stability analysis of a two dimensional laminar airfoil with two degrees-of-freedom ...
First results of a flutter experiment in transonic flow are presented. A wind tunnel model with the ...
A laminar wing test case for the flutter behavior in transonic flow with free boundary layer transit...
The flutter behavior of a supercritical airfoil is investigated using a panel formulation, which sol...
The steady flow aerodynamics of a cascade of compressor airfoils is computed using a two-dimensional...
Angle of attack has impact on transonic flow filed and aerodynamic force, but most of current resear...