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Numerical Study of the Influence of Deformation on Transition and Hysteresis Behaviour of Separation Mechanisms in Thrust-Optimized Parabolic Rocket Nozzles

Smolka, Nadine (2018) Numerical Study of the Influence of Deformation on Transition and Hysteresis Behaviour of Separation Mechanisms in Thrust-Optimized Parabolic Rocket Nozzles. Master's, Technische Universität Berlin.

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Item URL in elib:https://elib.dlr.de/124309/
Document Type:Thesis (Master's)
Title:Numerical Study of the Influence of Deformation on Transition and Hysteresis Behaviour of Separation Mechanisms in Thrust-Optimized Parabolic Rocket Nozzles
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Smolka, NadineUNSPECIFIEDUNSPECIFIED
Date:21 November 2018
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Numerical Simulation, Deformation, Transition, Hysteresis Behavior, TOP Nozzles
Institution:Technische Universität Berlin
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):Proj TAUROS (TAU for Rocket Thrust Chamber Simulation)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Steinberg, Silke
Deposited On:12 Dec 2018 10:05
Last Modified:12 Dec 2018 10:05

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