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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Stark, Ralf	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2005

Refereed publication:

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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 Start Date:

10 July 2005

Event End Date:

13 July 2005

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:

24 Apr 2024 19:11

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