The reliable prediction of low-speed flow separation of a turbulent boundary layer on a smooth surface due to an adverse pressure gradient is still an open issue. In the literature, there is no agreement on a law-of-the-wall in case of an adverse pressure gradient. We present a recent and ongoing research investigation started in the DLR internal project RETTINA is to build up a worldwide unique set of experimental data for a turbulent boundary layer flow at adverse pressure gradient obtained by a joint large-scale PIV campaign of DLR and UniBw München, and to investigate existing and to develop improved proposals for the law-of-the-wall in case of an adverse pressure gradient
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
Flow separation of turbulent boundary layer flow on a smooth surface due to an adverse pressure grad...
The reliable prediction of low-speed flow separation of a turbulent boundary layer (TBL) on a smooth...
We present an experimental investigation of a turbulent boundary layer flow at adverse pressure grad...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a ...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a s...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a s...
subjected to a streamwise adverse pressure gradient Δp+ =ν/(ρu3 τ) dp/dx. However the statistically...
We present the design of a dedicated experiment and first results from corresponding PIV measurement...
With an ever increasing need for drag and in turn emission reduction, flow control concepts aiming t...
A new experiment of a turbulent boundary layer flow at a large adverse pressure gradient at a high R...
A modification of the SSG/LRR-omega model for turbulent boundary layers in adverse pressure gradient...
Wall-bounded turbulence is present in many relevant fluid-flow problems such as the flow around wing...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
Flow separation of turbulent boundary layer flow on a smooth surface due to an adverse pressure grad...
The reliable prediction of low-speed flow separation of a turbulent boundary layer (TBL) on a smooth...
We present an experimental investigation of a turbulent boundary layer flow at adverse pressure grad...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a ...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a s...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
We present an experimental investigation and data analysis of a turbulent boundary layer flow at a s...
subjected to a streamwise adverse pressure gradient Δp+ =ν/(ρu3 τ) dp/dx. However the statistically...
We present the design of a dedicated experiment and first results from corresponding PIV measurement...
With an ever increasing need for drag and in turn emission reduction, flow control concepts aiming t...
A new experiment of a turbulent boundary layer flow at a large adverse pressure gradient at a high R...
A modification of the SSG/LRR-omega model for turbulent boundary layers in adverse pressure gradient...
Wall-bounded turbulence is present in many relevant fluid-flow problems such as the flow around wing...
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse...
Flow separation of turbulent boundary layer flow on a smooth surface due to an adverse pressure grad...
The reliable prediction of low-speed flow separation of a turbulent boundary layer (TBL) on a smooth...