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Hot film and PIV measurements at propeller thrust reverse

Roosenboom, Eric and Kreplin, Hans-Peter and Schröder, Andreas (2007) Hot film and PIV measurements at propeller thrust reverse. ODAS 2007 - 8th ONERA-DLR Aerospace Symposium, 2007-10-17 - 2007-10-19, Göttingen (Germany).

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The flow around an 8-bladed propeller at thrust reverse conditions is analysed using stereoscopic Particle Image Velocimetry (PIV) and hot film sensors in the Airbus Low-Speed Wind Tunnel facility in Bremen, Germany. The propeller is mounted on a half-model equipped with two counter-rotating propellers, where only the outboard propeller is investigated. The model is equipped with landing configuration settings at an angle of incidence of 0° and flaps extended. The objective is to compare the signals obtained on the wing surface with hot film sensors with flow information ob-tained with PIV directly behind the outboard propeller at thrust reverse.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Hot film and PIV measurements at propeller thrust reverse
AuthorsInstitution or Email of Authors
Roosenboom, EricUNSPECIFIED
Kreplin, Hans-PeterUNSPECIFIED
Schröder, AndreasUNSPECIFIED
Refereed publication:No
In ISI Web of Science:No
Page Range:pp. 1-10
Series Name:Conference Proceedings
Keywords:PIV, Hot Film, Propeller flow, Thrust reverse, Industrial wind tunnel
Event Title:ODAS 2007 - 8th ONERA-DLR Aerospace Symposium
Event Location:Göttingen (Germany)
Event Type:international Conference
Event Dates:2007-10-17 - 2007-10-19
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:13 Nov 2007
Last Modified:27 Apr 2009 14:07

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