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Fluid Injection Process in High Pressure H2/O2 Rocket Engines: derived models and numerical simulations

Krülle, G. and Schley, C.-A. (1995) Fluid Injection Process in High Pressure H2/O2 Rocket Engines: derived models and numerical simulations. 11th European Conference of ILASS on Atomization and Sprays, Nuernberg, 21-23.03.1995.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/24916/
Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=Nuernberger Messe GmbH, LIDO-Berichtsjahr=1995, pages=10,
Title:Fluid Injection Process in High Pressure H2/O2 Rocket Engines: derived models and numerical simulations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Krülle, G.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schley, C.-A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1995
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:partec 95
Status:Published
Keywords:Fluid Injection, Coaxial Injector, Supercritical, Conditious, Injection model, Numerical Simulation
Event Title:11th European Conference of ILASS on Atomization and Sprays, Nuernberg, 21-23.03.1995
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:37

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