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

Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames

Oschwald, M. and Cuoco, F. and Yang, B. and De Rosa, M. (2005) Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames. International Symposium on Heat and Mass Transfer in Spray Systems, 2005-06-05 - 2005-06-10, Anatalya (Turkey).

[img]
Preview
PDF
996kB
[img]
Preview
PDF
4MB

Abstract

Propellant injectors are for several reasons of central importance for the performance of rocket combustors. Existing correlations used to guide the design of injectors are mainly based on experimental und theoretical investigations of non-reacting sprays. Furthermore most of the experiments have been done with substitute fluids of significantly different properties as compared to liquid oxygen. Experimental investigations of reactive sprays with original propellants, liquid oxygen as oxidizer and hydrogen and methane as fuels, are presented and the influence of the injection conditions and of the fuel on the atomization and spray flame is discussed.

Item URL in elib:https://elib.dlr.de/53333/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Oschwald, M.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Cuoco, F.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Yang, B.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
De Rosa, M.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2005
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket propulsion
Event Title:International Symposium on Heat and Mass Transfer in Spray Systems
Event Location:Anatalya (Turkey)
Event Type:international Conference
Event Start Date:5 June 2005
Event End Date:10 June 2005
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 - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Oschwald, Dr.rer.nat. Michael
Deposited On:16 Feb 2008
Last Modified:24 Apr 2024 19:16

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.