DocumentCode
2546814
Title
Standalone trailing probe for aerometrical measurements
Author
Paces, Pavel ; Popelka, Jan ; Auersvald, J.
Author_Institution
Czech Tech. Univ. in Prague, Prague, Czech Republic
fYear
2012
fDate
14-18 Oct. 2012
Firstpage
1
Lastpage
1
Abstract
The paper presents the sensor evaluated by DRUCK GE6000 automated pressure controller for wind tunnel tests. The total port almost independent on AOA (and AOS). The probe head dP/Pc ratio reaches 1.6. There is negligible deviation between the probe measurement system and laboratory measurement instruments. The total absolute error after calibration is +/6 Pa.
Keywords
aircraft instrumentation; altimeters; velocity measurement; wind tunnels; DRUCK GE6000 automated pressure controller; aerometrical measurements; air speed indicator; altimeter; standalone trailing probe; wind tunnel test;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location
Williamsburg, VA
ISSN
2155-7195
Print_ISBN
978-1-4673-1699-6
Type
conf
DOI
10.1109/DASC.2012.6382946
Filename
6382946
Link To Document