Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
In: Berlin, Germany : Deutsche Gesellschaft für Akustik, 2019
- Event
-
Veröffentlichung
- (where)
-
Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2019
- Creator
-
Le, Hao
Wang, Yingchen
Chen, Jun
Shi, Xiaoming
- DOI
-
10.18154/RWTH-CONV-238985
- URN
-
urn:nbn:de:101:1-2020073114010643602567
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:47 PM CET
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Le, Hao
- Wang, Yingchen
- Chen, Jun
- Shi, Xiaoming
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2019
Other Objects (12)
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
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber
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
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
Testing the limits of the cryogenic nucleation pulse chamber
Unsteady Effects on NOx Measurements in Pulse Detonation Combustion
Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
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
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber
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
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
Testing the limits of the cryogenic nucleation pulse chamber
Unsteady Effects on NOx Measurements in Pulse Detonation Combustion
Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
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
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Pseudo-transient 3D Conjugate Heat Transfer Simulation and Lifetime Prediction of a Rocket Combustion Chamber
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
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
Testing the limits of the cryogenic nucleation pulse chamber
Unsteady Effects on NOx Measurements in Pulse Detonation Combustion
Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers