Hochschulschrift

Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling

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Location: Deutsche Nationalbibliothek Frankfurt am Main

ISBN: 9783844031348

Dimensions: 21 cm, 212 g

Extent: II, 129 S.

Language: Englisch

Notes: Ill., graph. Darst.
Zugl.: Aachen, Techn. Hochsch., Diss., 2014

Bibliographic citation: Applied mechanics ; Vol. 1

Keyword: Raketentriebwerk
Brennkammer
Kühlsystem
Auskleidung
Kupferlegierung
Duktilität
Viskoplastizität
Werkstoffschädigung
Lebensdauer
Prognosemodell

Event: Veröffentlichung

(where): Aachen

(who): Shaker

(when): 2014

Creator: Tini, Vivian

Table of contents: https://d-nb.info/105971373X/04

Rights: Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.

Last update: 11.06.2025, 1:57 PM CEST

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Object type

Hochschulschrift

Associated

Tini, Vivian
Shaker

Time of origin

2014

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Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

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Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning

Local anomaly detection in hybrid rocket combustion tests

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Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

Analysis and Improvement of Rocket Engine Combustion Stability Simulations

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber

Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks

Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks

Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber

Numerical Study on Wall Heat Flux in Film Cooling of Methane/Oxygen Rocket Engine Combustion Chamber

Turbulent Combustion Phenomena in Methane Rocket Engines

Hochschulschrift

Combustion phenomena of advanced hybrid rocket fuels

Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning

Local anomaly detection in hybrid rocket combustion tests

Hochschulschrift

Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

Analysis and Improvement of Rocket Engine Combustion Stability Simulations

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

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Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling

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Other Objects (12)

Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber

Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks

Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks

Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber

Numerical Study on Wall Heat Flux in Film Cooling of Methane/Oxygen Rocket Engine Combustion Chamber

Turbulent Combustion Phenomena in Methane Rocket Engines

Combustion phenomena of advanced hybrid rocket fuels

Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning

Local anomaly detection in hybrid rocket combustion tests

Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

Analysis and Improvement of Rocket Engine Combustion Stability Simulations

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber

Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks

Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks

Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber

Numerical Study on Wall Heat Flux in Film Cooling of Methane/Oxygen Rocket Engine Combustion Chamber

Turbulent Combustion Phenomena in Methane Rocket Engines

Combustion phenomena of advanced hybrid rocket fuels

Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning

Local anomaly detection in hybrid rocket combustion tests

Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

Analysis and Improvement of Rocket Engine Combustion Stability Simulations

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber

Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks

Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks

Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber

Numerical Study on Wall Heat Flux in Film Cooling of Methane/Oxygen Rocket Engine Combustion Chamber

Turbulent Combustion Phenomena in Methane Rocket Engines

Combustion phenomena of advanced hybrid rocket fuels

Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning

Local anomaly detection in hybrid rocket combustion tests

Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

Analysis and Improvement of Rocket Engine Combustion Stability Simulations

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

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