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Investigations to the Response Time of a Glued Thermocouple on the Basis of Experimental and Numerical Analyses

Barth, Tarik and Dankert, Carl and Roden, Günter von and Martinez Schramm, Jan (2010) Investigations to the Response Time of a Glued Thermocouple on the Basis of Experimental and Numerical Analyses. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer Verlag, Berlin Heidelberg. pp. 355-363. ISBN 978-3-642-14242-0. ISSN 1612-2909

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Official URL: http://www.springerlink.de/content/978-3-642-14242-0/?k=barth


Item URL in elib:https://elib.dlr.de/65245/
Document Type:Contribution to a Collection
Title:Investigations to the Response Time of a Glued Thermocouple on the Basis of Experimental and Numerical Analyses
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Barth, TarikUNSPECIFIEDUNSPECIFIED
Dankert, CarlUNSPECIFIEDUNSPECIFIED
Roden, Günter vonUNSPECIFIEDUNSPECIFIED
Martinez Schramm, JanUNSPECIFIEDUNSPECIFIED
Date:2 October 2010
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics VII
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:112
DOI :10.1007/978-3-642-14243-7_44
Page Range:pp. 355-363
Editors:
EditorsEmail
Dillmann, AndreasUNSPECIFIED
Heller, GerdAirbus Deutschland
Klaas, MichaelRWTH Aachen
Kreplin, Hans-PeterUNSPECIFIED
Nitsche, WolfgangTU Berlin
Schröder, WolfgangRTWH Aachen
Publisher:Springer Verlag, Berlin Heidelberg
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-642-14242-0
Status:Published
Keywords:Response Time, SHEFEX, Thermocouple
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - SHEFEX Programm (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Barth, Tarik
Deposited On:25 Oct 2010 14:08
Last Modified:27 Feb 2015 12:19

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