- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1868-2510
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Investigation of the base flow of a generic space launcher with dual-bell nozzle ; day:19 ; month:9 ; year:2020 ; pages:1-20
CEAS space journal / Confederation of European Aerospace Societies ; (19.9.2020), 1-20
- Creator
- Contributor
-
SpringerLink (Online service)
- DOI
-
10.1007/s12567-020-00333-5
- URN
-
urn:nbn:de:101:1-2020110816581150154945
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:24 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Scharnowski, Sven
- Kähler, Christian J.
- SpringerLink (Online service)
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Influence of nozzle parameters on spray pattern and droplet characteristics for a two-fluid nozzle
Nozzle temperature calibration in 3D printing
Duale Basen nulldimensionaler Ideale und Anwendungen
On the performance increase of future space launchers: Investigations of buffeting, its reduction via passive flow control, and the Dual-Bell nozzle concept at trans- and supersonic flight conditions
Simultaneous microscopic investigation of nozzle internal flow and primary breakup using a transparent high-pressure nozzle
Numerical investigation of nozzle base flow interaction of a generic space vehicle
Dual-nozzle microfluidic droplet generator
Numerical Analysis of Side-loads Reduction in a Sub-scale Dual-bell Rocket Nozzle
Semi‐Woven Structures via Dual Nozzle Melt Electrowriting
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Influence of Nozzle Parameters on Spray Pattern and Droplet Characteristics for a Two‐Fluid Nozzle
Influence of nozzle parameters on spray pattern and droplet characteristics for a two-fluid nozzle
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Duale Basen nulldimensionaler Ideale und Anwendungen
On the performance increase of future space launchers: Investigations of buffeting, its reduction via passive flow control, and the Dual-Bell nozzle concept at trans- and supersonic flight conditions