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Simultaneous density and velocity measurement for rotorcraft research in a transonic wind tunnel

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.

Full text not available from this repository.

Abstract

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
Authors:
AuthorsInstitution or Email of Authors
Richard, HughesUNSPECIFIED
Geissler, WolfgangUNSPECIFIED
Raffel, MarkusUNSPECIFIED
Date:2001
Journal or Publication Title:CD: 27th European Rotorcraft -Forum
Page Range:29.1-29.10
Status:Published
Keywords:density; velocity; rotorcraft; transonic.
Event Title:27th European Rotorcraft -Forum, Moscow, September 2001.
Event Location:Moscow
Event Type:international Conference
Event Dates:2001-10-29
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)
Location: Göttingen
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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