Richard, Hughes and Geissler, Wolfgang and Raffel, Markus (2001) Simultaneous density and velocity measurement for rotorcraft research in a transonic wind tunnel. In: CD: 27th European Rotorcraft -Forum, 29.1-29.10. 27th European Rotorcraft -Forum, Moscow, September 2001., 2001-10-29, Moscow.
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In recent years numerical codes based on the ime-eccurate solution of the Reynolds Averaged Navier-Stokes equations (RANS) have been developed. Results from these codes are ready for comparison with experimental data. A section of the present paper is dedicated to the comparison of numerical with corresponding experimental data.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Simultaneous density and velocity measurement for rotorcraft research in a transonic wind tunnel|
|Journal or Publication Title:||CD: 27th European Rotorcraft -Forum|
|Keywords:||density; velocity; rotorcraft; transonic.|
|Event Title:||27th European Rotorcraft -Forum, Moscow, September 2001.|
|Event Type:||international Conference|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Rotorcraft|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L RR - Rotorcraft Research|
|DLR - Research theme (Project):||L - The Active Rotorcraft (old)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Helicopters|
Institute of Aerodynamics and Flow Technology > High Speed Configurations
|Deposited By:||Ilka Micknaus|
|Deposited On:||29 Aug 2007|
|Last Modified:||14 Jan 2010 21:00|
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