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Half Model and Flow Visualisation Measurement Technique in Use at Kryo-Kanal Koeln (KKK).

Stahl, B. (1996) Half Model and Flow Visualisation Measurement Technique in Use at Kryo-Kanal Koeln (KKK). In: DEA AF-71-G-7425 Wind Tunnels and Flight Simulation Facilities Symposium, DLR Göttingen, 14.-15. Oktober 1996.

Full text not available from this repository.

Abstract

Force measurements with a heated half model balance and flow visualisation measurements were carried out on an Airbus half model at KKK. To detect the flow around the Airbus wing the following measuring techniques were used: - Visualisation of the wing flow by means of fluorescent mini-tufts - Visualisation of boundary layer effects on the wing by means of CO2 layer deposited on the wing surface and observation of CO2 sublimation.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996, pages=17,
Title:Half Model and Flow Visualisation Measurement Technique in Use at Kryo-Kanal Koeln (KKK).
Authors:
AuthorsInstitution or Email of Authors
Stahl, B.UNSPECIFIED
Date:1996
Journal or Publication Title:DEA AF-71-G-7425 Wind Tunnels and Flight Simulation Facilities Symposium, DLR Göttingen, 14.-15. Oktober 1996
Status:Published
Keywords:Force measurements, flow visualisation, mini-tufts, CO2 sublimation technique.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L SI - Versuchs- und Simulationstechniken
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:30

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