elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Heat Transfer in Porous Media Applied to Liquid Rocket Engines

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.

This is the latest version of this item.

Full text not available from this repository.

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/
Document Type:Conference or Workshop Item (Speech)
Title:Heat Transfer in Porous Media Applied to Liquid Rocket Engines
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Khamis, YacineUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Desmet, B.Univ. de Lille Nord de France, Valenciennes, FUNSPECIFIEDUNSPECIFIED
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

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.