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Analysis and prediction of the influence of high frequency combustion instabilities on heat transfer in a sub-scale LOX/H2 rocket thrust chamber

Govaert, Thomas (2019) Analysis and prediction of the influence of high frequency combustion instabilities on heat transfer in a sub-scale LOX/H2 rocket thrust chamber. Master's, University of Technology Delft, NL.

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Item URL in elib:https://elib.dlr.de/132954/
Document Type:Thesis (Master's)
Title:Analysis and prediction of the influence of high frequency combustion instabilities on heat transfer in a sub-scale LOX/H2 rocket thrust chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Govaert, ThomasDLR, Inst. für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIEDUNSPECIFIED
Date:2019
Refereed publication:No
Open Access:No
Number of Pages:118
Status:Published
Keywords:combustion instabilities, rocket propulsion, heat transfer
Institution:University of Technology Delft, NL
Department:Aerospace Engineering
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2019 16:07
Last Modified:18 Dec 2019 16:07

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