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Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle.

Hagemann, G. and Krülle, G. and Hannemann, K. (1996) Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle. AIAA Journal of Propulsion and Power, Vol.12,No.4.

Full text not available from this repository.

Abstract

Lampoldshausen 970219.

Item URL in elib:https://elib.dlr.de/25007/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1996, pages=7,
Title:Numerical Flowfield Analysis of the Next Generation Vulcan Nozzle.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hagemann, G.UNSPECIFIEDUNSPECIFIED
Krülle, G.UNSPECIFIEDUNSPECIFIED
Hannemann, K.UNSPECIFIEDUNSPECIFIED
Date:1996
Journal or Publication Title:AIAA Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol.12,No.4
Status:Published
Keywords:Nozzle, CFD, Turbine Exhaust Gas Injection, Vulcan Nozzle, Numerical Flowfield Analysis.
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 05:40

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