The NASA Juncture Flow experiment is a new effort whose focus is attaining validation data in the juncture region of a wing-body configuration. The experiment is designed specifically for the purpose of CFD validation. Current turbulence models routinely employed by Reynolds-averaged Navier-Stokes CFD are inconsistent in their prediction of corner flow separation in aircraft juncture regions, so experimental data in the near-wall region of such a configuration will be useful both for assessment as well as for turbulence model improvement. This paper summarizes the Juncture Flow effort to date, including preliminary risk-reduction experiments already conducted and planned future experiments. The requirements and challenges associated with co...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
Current turbulence models, such as those employed in Reynolds-averaged Navier-Stokes CFD, are unable...
Values of three mean velocity components and six turbulence stresses measured in a juncture flow are...
NASA has been working toward designing and conducting a juncture flow experiment on a wing-body airc...
The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separat...
NASAs Transformational Tools and Technologies Project (T(cu.) is supporting a substantial effort to ...
NASAs Transformational Tools and Technologies Programs Juncture Flow experiment aims to provide data...
Wing-body juncture flow fields on commercial aircraft configurations are challenging to compute accu...
Because future wind tunnel tests associated with the NASA Juncture Flow project are being designed f...
A wing/fuselage wind-tunnel model was tested in the Langley 14- by 22-foot Subsonic Wind Tunnel in p...
This paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Comput...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
Values of three mean velocity components and six turbulence stresses measured in a turbulent shear l...
As identified in the CFD Vision 2030 Study commissioned by NASA, validation of advanced RANS models ...
With computational fluid dynamics (CFD) becoming a productive research and design tool, the requirem...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
Current turbulence models, such as those employed in Reynolds-averaged Navier-Stokes CFD, are unable...
Values of three mean velocity components and six turbulence stresses measured in a juncture flow are...
NASA has been working toward designing and conducting a juncture flow experiment on a wing-body airc...
The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separat...
NASAs Transformational Tools and Technologies Project (T(cu.) is supporting a substantial effort to ...
NASAs Transformational Tools and Technologies Programs Juncture Flow experiment aims to provide data...
Wing-body juncture flow fields on commercial aircraft configurations are challenging to compute accu...
Because future wind tunnel tests associated with the NASA Juncture Flow project are being designed f...
A wing/fuselage wind-tunnel model was tested in the Langley 14- by 22-foot Subsonic Wind Tunnel in p...
This paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Comput...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
Values of three mean velocity components and six turbulence stresses measured in a turbulent shear l...
As identified in the CFD Vision 2030 Study commissioned by NASA, validation of advanced RANS models ...
With computational fluid dynamics (CFD) becoming a productive research and design tool, the requirem...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
Current turbulence models, such as those employed in Reynolds-averaged Navier-Stokes CFD, are unable...
Values of three mean velocity components and six turbulence stresses measured in a juncture flow are...