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.

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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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
van der Wall, Berend G.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Richard, Hugues	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

8 May 2008

Refereed publication:

Open Access:

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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