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Development of a Stability Rating Device for Sub-Scale Liquid Propellant Rocket Combustors

Häring, Sebastian (2019) Development of a Stability Rating Device for Sub-Scale Liquid Propellant Rocket Combustors. Master's, Aachen University of Applied Sciences.

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Item URL in elib:https://elib.dlr.de/132945/
Document Type:Thesis (Master's)
Title:Development of a Stability Rating Device for Sub-Scale Liquid Propellant Rocket Combustors
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Häring, SebastianDLR, Inst. für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Date:2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:117
Status:Published
Keywords:stability rating device, shock tube, ANSYS FLUENT, ANSYS Mechanical, Matlab, Shock Wave, CFD, FEA
Institution:Aachen University of Applied Sciences
Department:Institute of Applied Thermodynamics and Combustion Technology
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
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2019 16:05
Last Modified:18 Dec 2019 16:05

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