Add to ORKGThis paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Computational Fluid Dynamic analyses, on a wing-body configuration. The configuration is designed to produce regions of separation in the juncture where the wing meets the body. Detailed on- and off-body measurements in the juncture flow are compared with RANS predictions. The results from the experimental measurements will become part of a database of high fidelity measurements, to be used for calibration of turbulence models and validation of emerging computational prediction techniques
The predictive performance of several turbulence models, among them formulations based on non-linear...
Abstract Juncture flow and cavity flow are complex types of flow that are studied frequently because...
Values of three mean velocity components and six turbulence stresses measured in a turbulent shear l...
This paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Comput...
Wing-body juncture flow fields on commercial aircraft configurations are challenging to compute accu...
The NASA Juncture Flow experiment is a new effort whose focus is attaining validation data in the ju...
NASAs Transformational Tools and Technologies Project (T(cu.) is supporting a substantial effort to ...
The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separat...
NASA has been working toward designing and conducting a juncture flow experiment on a wing-body airc...
A wing/fuselage wind-tunnel model was tested in the Langley 14- by 22-foot Subsonic Wind Tunnel in p...
NASAs Transformational Tools and Technologies Programs Juncture Flow experiment aims to provide data...
Several experimental databases of aeroelastic measurements performed on aircraft wing models are ava...
Because future wind tunnel tests associated with the NASA Juncture Flow project are being designed f...
Vita.Influence of wing sweep on juncture flow has been investigated using three component laser Dopp...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
The predictive performance of several turbulence models, among them formulations based on non-linear...
Abstract Juncture flow and cavity flow are complex types of flow that are studied frequently because...
Values of three mean velocity components and six turbulence stresses measured in a turbulent shear l...
This paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Comput...
Wing-body juncture flow fields on commercial aircraft configurations are challenging to compute accu...
The NASA Juncture Flow experiment is a new effort whose focus is attaining validation data in the ju...
NASAs Transformational Tools and Technologies Project (T(cu.) is supporting a substantial effort to ...
The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separat...
NASA has been working toward designing and conducting a juncture flow experiment on a wing-body airc...
A wing/fuselage wind-tunnel model was tested in the Langley 14- by 22-foot Subsonic Wind Tunnel in p...
NASAs Transformational Tools and Technologies Programs Juncture Flow experiment aims to provide data...
Several experimental databases of aeroelastic measurements performed on aircraft wing models are ava...
Because future wind tunnel tests associated with the NASA Juncture Flow project are being designed f...
Vita.Influence of wing sweep on juncture flow has been investigated using three component laser Dopp...
Numerical simulations of the NASA Juncture Flow Experiment are carried out, employing a Reynolds-str...
The predictive performance of several turbulence models, among them formulations based on non-linear...
Abstract Juncture flow and cavity flow are complex types of flow that are studied frequently because...
Values of three mean velocity components and six turbulence stresses measured in a turbulent shear l...