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Bartolome Calvo, Javier and Hannemann, Klaus (2010) Analysis of the Heat Transfer in Liquid Rocket Engine Cooling Channels. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer-Verlag, Berlin Heidelberg. pp. 441-448. doi: 10.1007/978-3-642-14243-7_54. ISBN 978-3-642-14242-0. ISSN 1612-2909.
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Official URL: http://link.springer.com/chapter/10.1007%2F978-3-642-14243-7_54
Abstract
Simulations of supercritical nitrogen flow in cooling channels are compared with experimental results provided by EADS-Astrium Ottobrunn. The objective is to extend and validate the DLR-Tau code to compute and predict the heat transfer in cooling channels of liquid rocket engines. To simulate the flow accurately, the roughness of the surface, the thermophysical properties of the supercritical fluid, as well as the conduction in the structure are modeled.
| Item URL in elib: | https://elib.dlr.de/96032/ | ||||||||||||||||||||||||||||
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| Document Type: | Contribution to a Collection | ||||||||||||||||||||||||||||
| Title: | Analysis of the Heat Transfer in Liquid Rocket Engine Cooling Channels | ||||||||||||||||||||||||||||
| Authors: |
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| Date: | 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_54 | ||||||||||||||||||||||||||||
| Page Range: | pp. 441-448 | ||||||||||||||||||||||||||||
| Editors: |
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| 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: | DLR-Tau code, supercritical fluid, Liquid Rocket Engine | ||||||||||||||||||||||||||||
| 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 - Grundlagen Raumtransport - numerische Verfahren (old) | ||||||||||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||||||||||||||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||||||||||||||||||
| Deposited On: | 21 Apr 2015 08:21 | ||||||||||||||||||||||||||||
| Last Modified: | 21 Apr 2015 08:21 |
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