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Numerical investigation of Dual Bell Nozzle Flow Field

Génin, Chloe and Stark, Ralf and Karl, Sebastian and Schneider, Dirk (2012) Numerical investigation of Dual Bell Nozzle Flow Field. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 29. Jul. - 1. Aug 2012, Atlanta, GA, USA. DOI: 10.2514/6.2012-4164.

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Official URL: https://www.aiaa.org/

Abstract

The flow field of a cold flow dual bell has been numerically simulated with the DLR TAU code. The two operation modes and the transition from one mode to the other are investigated by varying the nozzle pressure ratio. A cold flow test campaign on a sub-scale nozzle model yields experimental data for validation of the simulation. Pressure measurements along the nozzle wall and schlieren optics provides information on the flow field in the nozzle. In addition, the models have been successively shortened to allow the observation of the shock system in the vicinity of the contour inflection.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Numerical investigation of Dual Bell Nozzle Flow Field
Authors:
AuthorsInstitution or Email of Authors
Génin, ChloeChloe.Genin@dlr.de
Stark, RalfRalf.Stark@dlr.de
Karl, SebastianSebastian.Karl@dlr.de
Schneider, DirkDirk.Schneider@dlr.de
Date:2012
Refereed publication:No
In ISI Web of Science:No
DOI:10.2514/6.2012-4164
Series Name:Conference Proceedings onloine
Status:Published
Keywords:nozzle flow, dual bell nozzle, CFD
Event Title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:29. Jul. - 1. Aug 2012
Organizer:American Institute of Aeronautics and Astronautics (AIAA)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Space Propulsion > Raketenantriebe
Deposited By: Chloe Nürnberger-Genin
Deposited On:08 Oct 2012 20:33
Last Modified:12 Dec 2013 21:47

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