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Theoretical Investigations of Droplet Flow under Typical Coaxial Injector Flow Conditions in Cryogenic Rocket Engines.

Krülle, G. and Labani, R. (1) and Mayer, W. (1992) Theoretical Investigations of Droplet Flow under Typical Coaxial Injector Flow Conditions in Cryogenic Rocket Engines. In: Proceedings AIAA 28th Joint Propulsion Conference. AIAA; 28th Joint Propulsion Conference; Nashville; TN; USA; 1992.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/24752/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1993, pages=13,
Title:Theoretical Investigations of Droplet Flow under Typical Coaxial Injector Flow Conditions in Cryogenic Rocket Engines.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krülle, G.UNSPECIFIEDUNSPECIFIED
Labani, R. (1)UNSPECIFIEDUNSPECIFIED
Mayer, W.UNSPECIFIEDUNSPECIFIED
Date:1992
Journal or Publication Title:Proceedings AIAA 28th Joint Propulsion Conference
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA 92-3121
Status:Published
Keywords:Treibstoffaufbereitung, Chemische Antriebe, Tropfenstroemung, numerische Spraysimulation
Event Title:AIAA; 28th Joint Propulsion Conference; Nashville; TN; USA; 1992
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):UNSPECIFIED
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Institut für Chemische Antriebe und Verfahrenstechnik
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:34

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