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Hover Tip Vortex Structure Test (HOTIS) - Test Documentation and Representative Results -

van der Wall, Berend G. and Richard, Hugues (2008) Hover Tip Vortex Structure Test (HOTIS) - Test Documentation and Representative Results -. DLR-Interner Bericht. DLR-IB 111-2008/16, 144 S.

Full text not available from this repository.

Abstract

With data from this HOTIS test, performed 2005 in the rotor preparation hall of DLR Inst. of Flight Systems together with the PIV experts of the DLR Inst. of Aerodynamics and Flow Technology the final proof of the advantages of PIV compared to LDV was aimed to be given. The publications of the results already showed that this proof was successful. This report describes in detail the test setup, the measurement equipment used and results obtained.

Item URL in elib:https://elib.dlr.de/54109/
Document Type:Monograph (DLR-Interner Bericht)
Title:Hover Tip Vortex Structure Test (HOTIS) - Test Documentation and Representative Results -
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van der Wall, Berend G.UNSPECIFIEDUNSPECIFIED
Richard, HuguesUNSPECIFIEDUNSPECIFIED
Date:8 May 2008
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:144
Status:Published
Keywords:Vortex flow field, rotor tip vortex, PIV
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Active Rotorcraft (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Aerodynamics and Flow Technology > Fluid Systems
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:14 Jan 2009
Last Modified:27 Apr 2009 14:56

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