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A Numerical Model for Nozzle Flow Application under LOX/CH4 Hot Flow Conditions

Schneider, Dirk and Génin, Chloé and Karl, Sebastian and Hannemann, Volker (2016) A Numerical Model for Nozzle Flow Application under LOX/CH4 Hot Flow Conditions. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 25.-27. Juli 2016, Salt Lake City, Utah, USA. DOI: 10.2514/6.2016-4671

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Item URL in elib:https://elib.dlr.de/107794/
Document Type:Conference or Workshop Item (Speech)
Title:A Numerical Model for Nozzle Flow Application under LOX/CH4 Hot Flow Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schneider, DirkDirk.Schneider (at) dlr.deUNSPECIFIED
Génin, ChloéChloe.Genin (at) dlr.deUNSPECIFIED
Karl, SebastianSebastian.Karl (at) dlr.deUNSPECIFIED
Hannemann, VolkerVolker.Hannemann (at) dlr.deUNSPECIFIED
Date:27 July 2016
Journal or Publication Title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2016-4671
Status:Published
Keywords:nozzle flow, dual-bell nozzle, numerical nozzle flow Simulation, methane combustion
Event Title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
Event Location:Salt Lake City, Utah, USA
Event Type:international Conference
Event Dates:25.-27. Juli 2016
Organizer: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 - ProTAU + Prop2020 Hochleistungstriebwerke
Location: Göttingen , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:50
Last Modified:31 Jul 2019 20:04

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