Add to ORKG19 ABSTRACT (Continue on reverse if necessary and identify by block number) Thie dynamic stall of rapidly pitching and oscillating airfoils is investigated by the numerical solution of the full compressible unsteady two-dimensional Navier-Stokes equa-tions using an alternating-direction-implicit scheme. The flow is assumend to be fully turbulent, and the turbulent stresses are modelled by the Baldwin-Lomax eddy viscosit
Computations for two-dimensional flow past a stationary and harmonically pitching wind turbine airfo...
Numerical experiments are conducted to simulate airfoils pitching up at constant rates into the dyna...
The article of record as published may be found at https://doi.org/The article of record as publishe...
19 ABSTRACT (Continue on reverse if necessary and identify by block number) Thie dynamic stall of ra...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1991-1798The dynamic ...
© 1998, American Institute of Aeronautics and Astronautics, Inc.The dynamic stall boundaries of a NA...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1998-2519The dynamic ...
This article demonstrates the conception of numerical techniques for simulating the flow around a NA...
International audienceThe fluid structure interaction due to the pitching motion of a NACA0012 aerof...
Computer Physics Communications, Elsevier Science Publishers, B.V., Vol. 65(1991), pp. 62-68.Results...
Abstract—The term dynamic stall refers to unsteady flow separation occurring on aerodynamic bodies, ...
This report summarizes the key results from the two components of the study: (1) development of the ...
A computational approach is described for the rapid and systematic prediction and evaluation of the ...
ABSTRACT: In this research, viscous, unsteady and turbulent fluid flow is simulated numerically arou...
An interactive boundary layer model has been developed and coupled with a pitch plunge airfoil in 2d...
Computations for two-dimensional flow past a stationary and harmonically pitching wind turbine airfo...
Numerical experiments are conducted to simulate airfoils pitching up at constant rates into the dyna...
The article of record as published may be found at https://doi.org/The article of record as publishe...
19 ABSTRACT (Continue on reverse if necessary and identify by block number) Thie dynamic stall of ra...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1991-1798The dynamic ...
© 1998, American Institute of Aeronautics and Astronautics, Inc.The dynamic stall boundaries of a NA...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1998-2519The dynamic ...
This article demonstrates the conception of numerical techniques for simulating the flow around a NA...
International audienceThe fluid structure interaction due to the pitching motion of a NACA0012 aerof...
Computer Physics Communications, Elsevier Science Publishers, B.V., Vol. 65(1991), pp. 62-68.Results...
Abstract—The term dynamic stall refers to unsteady flow separation occurring on aerodynamic bodies, ...
This report summarizes the key results from the two components of the study: (1) development of the ...
A computational approach is described for the rapid and systematic prediction and evaluation of the ...
ABSTRACT: In this research, viscous, unsteady and turbulent fluid flow is simulated numerically arou...
An interactive boundary layer model has been developed and coupled with a pitch plunge airfoil in 2d...
Computations for two-dimensional flow past a stationary and harmonically pitching wind turbine airfo...
Numerical experiments are conducted to simulate airfoils pitching up at constant rates into the dyna...
The article of record as published may be found at https://doi.org/The article of record as publishe...