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Numerical and Experimental Study of the Flow in a Planar Expansion-Deflection Nozzle

Wagner, Bernd and Schlechtriem, S. (2011) Numerical and Experimental Study of the Flow in a Planar Expansion-Deflection Nozzle. In: Proceedings (AIAA 2011-5942). 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 31. Jul. - 3. Aug. 2011, San Diego, California, USA.

Full text not available from this repository.

Abstract

Wall pressure measurements and schlieren images gained from cold flow test with a generic planar expansion-deflection nozzle at various nozzle pressure ratios are compared to numerical simulations with the DLR TAU code. The nozzle geometry is simulated on 2d and 3d meshes. The focus is on simulations on 3d meshes, to capture the flow effects during the experiments. Several meshes and three turbulence models are computed for different NPR and the wall pressure distribution in the wake region is taken for the comparison. For two selected grids an incremental increase and decrease of the pressure ratio range from 10 to 25 is simulated. Thus, the transition behavior and a hysteresis are studied numerically.

Item URL in elib:https://elib.dlr.de/72180/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Numerical and Experimental Study of the Flow in a Planar Expansion-Deflection Nozzle
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wagner, BerndBernd.Wagner (at) dlr.deUNSPECIFIED
Schlechtriem, S.Stefan.Schlechtriem (at) dlr.deUNSPECIFIED
Date:2011
Journal or Publication Title:Proceedings
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:numerical simulation, numerical simulation
Event Title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Event Location:San Diego, California, USA
Event Type:international Conference
Event Dates:31. Jul. - 3. Aug. 2011
Organizer:AIAA
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: Hanke, Michaela
Deposited On:01 Dec 2011 12:11
Last Modified:01 Dec 2018 19:47

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