Khamis, Yacine and Suslov, Dmitry and Desmet, B. (2013) Heat Transfer in Porous Media Applied to Liquid Rocket Engines. In: Proceedings EUCASS. 5th EUCASS, 2013-07-01 - 2013-07-05, München, Deutschland.
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Abstract
Advances in space propulsion require the use of new materials. The Institute of Space Propulsion at DLR Lampoldshausen (Germany) has been investigating for the application of porous materials in liquid rocket engines. The development of transpiration cooling for combustion chamber is based on such materials in a configuration where hydrogen flows through the wall. Another application is injector heads which offer a better homogenization of the propellants. The efficiency and reliability of such components depend on the permeability of the flow through the porous structure and the heat exchange between the fluid and the porous material. A description of those physical processes is necessary. A new experimental set up has been developed with requirements to reproduce and to control flow and heat transfer in a porous material at high temperature, high pressure and a wide range of mass flow. It gives the possibility to study the influence of the properties and the structure of the porous material, the properties of the fluid, the parameters of the flow and the heat loads. Appropriate measurements will be made in the fluid and on the material to determine the pressure loss and the thermal exchanges in the porous sample. The main objective is to develop appropriate models of permeability and heat transfer for real rocket components. This work presents the investigation made to develop such an experimental device. The design and the methodology of the measurements chosen are explained. First experimental results and CFD analysis are also given.
Item URL in elib: | https://elib.dlr.de/85061/ | ||||||||||||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||
Title: | Heat Transfer in Porous Media Applied to Liquid Rocket Engines | ||||||||||||||||
Authors: |
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Date: | 2013 | ||||||||||||||||
Journal or Publication Title: | Proceedings EUCASS | ||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||
Open Access: | No | ||||||||||||||||
Gold Open Access: | No | ||||||||||||||||
In SCOPUS: | No | ||||||||||||||||
In ISI Web of Science: | No | ||||||||||||||||
Status: | Published | ||||||||||||||||
Keywords: | heat transfer, transpiration cooling | ||||||||||||||||
Event Title: | 5th EUCASS | ||||||||||||||||
Event Location: | München, Deutschland | ||||||||||||||||
Event Type: | international Conference | ||||||||||||||||
Event Start Date: | 1 July 2013 | ||||||||||||||||
Event End Date: | 5 July 2013 | ||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||
HGF - Program: | Space | ||||||||||||||||
HGF - Program Themes: | Space Transportation | ||||||||||||||||
DLR - Research area: | Raumfahrt | ||||||||||||||||
DLR - Program: | R RP - Space Transportation | ||||||||||||||||
DLR - Research theme (Project): | R - Antriebsystemtechnik - Schubkammertechnologie (old) | ||||||||||||||||
Location: | Lampoldshausen | ||||||||||||||||
Institutes and Institutions: | Institute of Space Propulsion > Rocket Propulsion | ||||||||||||||||
Deposited By: | Hanke, Michaela | ||||||||||||||||
Deposited On: | 11 Nov 2013 08:57 | ||||||||||||||||
Last Modified: | 24 Apr 2024 19:51 |
Available Versions of this Item
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Untersuchung des Einflusses von Rauheit innerhalb von Rechteckkanälen bei asymmetrischer Wärmelast. (deposited 11 Nov 2013 08:54)
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Einfluss einer Kavität auf das Druckfeld der ersten Tangentialen Mode einer Raketenbrennkammer unter repräsentativen Bedingungen. (deposited 11 Nov 2013 08:48)
- Heat Transfer in Porous Media Applied to Liquid Rocket Engines. (deposited 11 Nov 2013 08:57) [Currently Displayed]
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Einfluss einer Kavität auf das Druckfeld der ersten Tangentialen Mode einer Raketenbrennkammer unter repräsentativen Bedingungen. (deposited 11 Nov 2013 08:48)
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