Acoustic Characteristics of Phase-Synchronized Adjacent Propellers
Airbus, Pressure Measurements on the Transonic Aerofoil RAE2822
Air jet flow control on pitching aerofoils
Wingtip Vortex structure in Swept-tapered wings
Two-Bladed Propeller Performance in Inclined Flow
Automotive DrivAer model – Fastback, Notchback, Estate back
Axisymmetric body
Windsor Automotive Reference Model
SAE 20 Degree Notchback Automotive Reference Model
The National Wind Tunnel Facility (NWTF) Experimental Database provides open access to high quality UK datasets from the aerospace and automotive sectors. The NWTF database simplifies access to wind tunnel experimental data allowing users to quickly locate and extract specific measurements.
Share your datasets
NWTF invites members and associates to contribute datasets to the platform. Simply provide your data and we will prepare the metadata for publication. By sharing your work, you can increase visibility, encourage collaboration, and advance experimental aerodynamics. Contact Dhamotharan Veerasamy, D.Veerasamy@lboro.ac.uk or the NWTF hub for more information.