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SGO ITD successfully tested a Liquid Skin Heat Exchanger in flight

Dannhauer, Axel and Bosbach, Johannes and Krajewski, Andre and Ziehm, Sebastian and Colberg, Carsten (2014) SGO ITD successfully tested a Liquid Skin Heat Exchanger in flight. [Other]

Full text not available from this repository.

Official URL: http://www.cleansky.eu/content/page/clean-sky-e-news


In September 2014, two flight tests of an experimental Liquid Skin Heat Exchanger (LSHX) have been carried out on the DLR Airbus A320 DATRA (Advanced Technology Research Aircraft). The LSHX test was embedded in a combined flight test campaign of the partners Airbus, Liebherr and DLR. As part of the thermal management stream in the SGO ITD, Liebherr‐Aerospace has developed and qualified this prototype heat exchanger and an experimental liquid loop system which was needed to simulate thermal cabin loads and to feed the LSHX with the cooling fluid on board of the test aircraft. Airbus was in charge of the aircraft integration and of the Flight Test Instrumentation. DLR was in charge to monitor, evaluate and analyse the A/C data as well as to determine the aerodynamic boundary conditions by means of boundary layer rake measurements.

Item URL in elib:https://elib.dlr.de/91243/
Document Type:Other
Additional Information:WP 4.4 Large scale demonstration
Title:SGO ITD successfully tested a Liquid Skin Heat Exchanger in flight
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Ziehm, SebastianLiebherrUNSPECIFIED
Colberg, CarstenAirbusUNSPECIFIED
Date:28 October 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:2
Series Name:CLEAN SKY e-news
Keywords:ATRA Flight Test, Heat Exchanger, Heat Transfer, Baindary Layer
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems and Cabin (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Fluid Systems
Flugexperimente > Forschungsflugabteilung Braunschweig
Deposited By: Micknaus, Ilka
Deposited On:05 Dec 2014 13:31
Last Modified:20 Jun 2021 15:45

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