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Flow Separation in Rocket Nozzles, a Simple Criteria

Stark, Ralf (2005) Flow Separation in Rocket Nozzles, a Simple Criteria. 41th Joint Propulsion Conference & Exhibit, 2005-07-10 - 2005-07-13, Tucson, Arizona (USA).

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Abstract

Cold and hot flow tests were conducted to investigate the flow separation in rocket nozzles. The results are presented. A separation data base including a wide range of literature data is established to evaluate the influence of propellant combination and nozzle design on flow separation. As a result a simple separation criteria is suggested.

Item URL in elib:https://elib.dlr.de/49253/
Document Type:Conference or Workshop Item (Paper)
Title:Flow Separation in Rocket Nozzles, a Simple Criteria
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Stark, RalfUNSPECIFIEDUNSPECIFIED
Date:2005
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Separation Criteria, Nozzle Flow, Flow Separation, Separation Data Base
Event Title:41th Joint Propulsion Conference & Exhibit
Event Location:Tucson, Arizona (USA)
Event Type:international Conference
Event Dates:2005-07-10 - 2005-07-13
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 - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Stark, Dr.-Ing. Ralf
Deposited On:03 Jul 2007
Last Modified:31 Jul 2019 19:19

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