There is a newer version of the record available.

Published May 11, 2023 | Version v.1.2.0
Dataset Open

H2020 ENODISE: UBRI Experimental Aeroacoustic Database BLI Configuration A

  • 1. University of Bristol
  • 2. Roma Tre University

Description

This database contains the datasets for the aeroacoustic experiments conducted at the University of Bristol regarding Boundary Layer Ingestion configurations A1 and A2 as part of the H2020 ENODISE project.

Configuration A1 consists of a propeller ingesting a zero-pressure-gradient boundary layer while A2 is a propeller ingesting an adverse pressure gradient boundary layer in a partially buried configuration. Far-field acoustics are measured using two microphone arcs, near-field measurements consist of surface static pressure and pressure fluctuations. Propeller force and torque is measured using a load cell. Flow-field measurements are obtained through hotwire anemometry.

This forms part of Deliverable D3.3, see D3.3 report for further information regarding measurement techniques. Included are descriptive READMEs and instrumentation layouts. The data is in the HDF5 format and comprises mean, spectral, and other processed data types in engineering units.

Now updated with D3.6 to include cleaned CAD models of both A1 and A2 configurations in STEP formats.

Notes

v1.0.1 - updated A2.UBRI.zip to correct static pressure rms calculation and hotwire SW Y coordinates. v1.1.0 - updated A2.UBRI.zip to more accurately reflect measured freestream velocities - replaced SW Plate Only hotwire data in A2.UBRI.zip with 2D X-wire counterparts, additional lines. - updated A1.UBRI.zip to more accurately reflect measured freestream velocities v1.2.0 - Added CAD geometry files

Files

A1.CAD Geometry.zip

Files (58.3 GB)

Name Size Download all
md5:19bd1e001929e8055a8af825eb70851d
12.5 MB Preview Download
md5:6cdbb9251f5e621d1b1a1b9a68bdda70
23.2 GB Preview Download
md5:03d1839cd80d9bd1995e697e57c6115f
9.1 MB Preview Download
md5:a773dcfd35f8d62007a57b0278e6a18d
35.0 GB Preview Download

Additional details

Funding

ENODISE – Enabling optimized disruptive airframe-propulsion integration concepts 860103
European Commission