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

Flow transition in dual bell nozzles

Nürnberger-Genin, Chloe and Stark, Ralf (2008) Flow transition in dual bell nozzles. Shock Waves Journal. Springer Berlin. DOI: 10.1007/s00193-008-0176-4 ISSN 0938-1287(Print) 1432-2153(Online)

Full text not available from this repository.

Official URL: http://www.springerlink.com/content/tg065068263j7118/


The dual bell nozzle is a concept of altitude adaptive nozzles. The flow adapts to the altitude by separation at the wall inflection at low altitude, and full flowing at high altitude. To understand the phenomenology of the flow by the transition from sea-level mode to high altitude mode, a series of tests have been made at the cold flow test bench P6.2 at DLR Lampoldshausen. A dual bell nozzle have been successively shorten and driven in the same conditions for each length. Hence it was possible to observe the flow in the vicinity of the wall inflection using Schlieren optics. Furthermore this study yields the influence of the length ratio between basis and extension on the transition conditions.

Item URL in elib:https://elib.dlr.de/57190/
Document Type:Article
Title:Flow transition in dual bell nozzles
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Date:20 November 2008
Journal or Publication Title:Shock Waves Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
DOI :10.1007/s00193-008-0176-4
Publisher:Springer Berlin
ISSN:0938-1287(Print) 1432-2153(Online)
Keywords:Nozzle, Dual bell, Experimental, Flow transition, Cold flow
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 - Raketenantriebtests (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Nürnberger-Genin, Chloe
Deposited On:11 Jan 2009
Last Modified:27 Apr 2009 15:40

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.