Dataset Open Access
Ceyhan Ozlem; Pires Oscar; Munduate Xabier
Within EU FP7 AVATAR project (AdVanced Aerodynamic Tools of lArge Rotors), a high Reynolds number and low Mach number wind tunnel test has been performed with the aim to obtain reliable data that can be used to validate existing aerodynamic models for this operating range. The test has been performed at the DNW High Pressure Wind Tunnel in Göttingen (HDG).
|AVATAR_blindTestCampaign_final.pdf md5:9fd21628087c446894fa0ccaad50c95b||1.5 MB||Download|
|Data.zip md5:3ebf32e958b53a6ed680155f7543aa9b||610.8 kB||Download|
|measuredCoordinates100mmFromMS_CASE1.txt md5:b340cc1025aec596ea0deb8e91563f45||3.3 kB||Download|
|nominalCoordinates_CASE1.txt md5:30f5c3aab5c960a8e6cfcce732bdf088||3.1 kB||Download|
|Test_description.docx md5:f18f8f454a6d454c35e19f2c80cf0070||26.7 kB||Download|