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This data has achieved Bronze level on 22 October 2015 which means this data makes a great start at the basics of publishing open data.

Low Speed Wind Tunnel Facility (LSWTF)

Summary

Type of release
a one-off release of a set of related datasets

Data Licence
Not Applicable

Content Licence
Creative Commons CCZero

Verification
automatically awarded

Release Date
15 October 2015
Modified Date
15 October 2015
Publishers
Federal Laboratory Consortium
Identifier
low-speed-wind-tunnel-facility-lswtf
Landing Page
http://catalog.data.gov/dataset/low-speed-wind-tunnel-facility-lswtf

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Description

Description: This facility consists of a large-scale, low-speed open-loop induction wind tunnel which has been modified to house a linear turbine cascade. A 125-hp electric motor powers an axial flow fan, drawing air at velocities up to 80m/s through an 85 cm by 122 cm test section. The entrance to the tunnel consists of a 3.0 m by 2.7 m rectangular bellmouth inlet. Honeycomb flow straighteners located in the inlet, combined with a gradual 8:1 area contraction, produce a uniform, low turbulence velocity profile at the cascade. Flow velocity uniformity is within ±1% with approximately 0.5% freestream turbulence. This level of turbulence can be augmented through the use of a turbulence-generating grid that produces freestream turbulence levels of approximately 4% at the cascade. The grid may also be fed with high-pressure air to produce turbulence levels of up to 15%. The inlet and test section pivot independently of the exit section, allowing the cascade inlet and exit to be set independently between 0° and 65°, allowing a total cascade turning of between 0° and 130°. The cascade is modular and can accommodate 85 cm span blades of up to 20 cm axial chord. A moving bar wake generator is available to provide periodic upstream unsteadiness over a wide range of reduced frequencies and flow coefficients. A modular splitter plate assembly may also be installed to allow the study of end-wall flows with controlled wall boundary layer conditions. Available instrumentation includes thermocouples, pressure probes, thermal anemometry, and Particle Image Velocimetry. Access is also available for use of a wide range of optical instrumentation techniques. Purpose: This facility is used to perform studies of turbine aerodynamics and flow control. Products: Low Reynolds number and high loading turbine component aerodynamics data. Data on the effects of periodic unsteadiness on turbine performance. Flow control data for application to turbine component design.


General Information


Legal Information

This dataset has been created by US Government which means it is required to be in the public domain. However US copyright law only allows open access by US citizens, we have assumed the data is equivalently licensed as CC0 for the rest of the world as this is in the spirit of the US Government’s Open Data policy.
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