Details
Original language | English |
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Title of host publication | New Results in Numerical and Experimental Fluid Mechanics XII |
Subtitle of host publication | Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018 |
Editors | Andreas Dillmann, Gerd Heller, Ewald Krämer, Claus Wagner, Cameron Tropea, Suad Jakirlić |
Pages | 427-436 |
Number of pages | 10 |
Edition | 1. |
ISBN (electronic) | 978-3-030-25253-3 |
Publication status | Published - 27 Sept 2019 |
Externally published | Yes |
Event | Symposium der Deutsche Gesellschaft für Luft- und Raumfahrt - Darmstadt, Germany Duration: 6 Nov 2018 → 7 Nov 2018 |
Publication series
Name | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
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Volume | 142 |
ISSN (Print) | 1612-2909 |
ISSN (electronic) | 1860-0824 |
Abstract
The system performance of a single-shaft turbojet engine is modelled with the pseudo bond graph approach in this paper. This theory is implemented in the in-house software tool ASTOR (AircraftEngine Simulation of Transient Operation Research) to simulate the overall dynamic of the turbojet model engine P200SX. In ASTOR, the transient performance is calculated with dynamic and individual control volumes to determine the three conservation equations. In this investigation a stationary operating point and a transient load case are simulated and compared to results of a commercial software and a measurement.
Keywords
- Bond graph theory, Gas turbine, Jet engine
ASJC Scopus subject areas
- Chemical Engineering(all)
- Fluid Flow and Transfer Processes
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New Results in Numerical and Experimental Fluid Mechanics XII: Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018. ed. / Andreas Dillmann; Gerd Heller; Ewald Krämer; Claus Wagner; Cameron Tropea; Suad Jakirlić. 1. ed. 2019. p. 427-436 Chapter 41 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design; Vol. 142).
Research output: Chapter in book/report/conference proceeding › Contribution to book/anthology › Transfer
}
TY - CHAP
T1 - System Dynamics of a Single-Shaft Turbojet Engine Using Pseudo Bond Graph
AU - Göing, Jan
AU - Kellersmann, Andreas
AU - Bode, Christoph
AU - Friedrichs, Jens
N1 - Funding information: The authors kindly thank the German Research Foundation (DFG) for the financial support to undergo the research project D6 “Interaction of combined module variances and influence on the overall system behavior” within the Collaborative Research Center (CRC) 871-Regeneration of Complex Capital Goods.
PY - 2019/9/27
Y1 - 2019/9/27
N2 - The system performance of a single-shaft turbojet engine is modelled with the pseudo bond graph approach in this paper. This theory is implemented in the in-house software tool ASTOR (AircraftEngine Simulation of Transient Operation Research) to simulate the overall dynamic of the turbojet model engine P200SX. In ASTOR, the transient performance is calculated with dynamic and individual control volumes to determine the three conservation equations. In this investigation a stationary operating point and a transient load case are simulated and compared to results of a commercial software and a measurement.
AB - The system performance of a single-shaft turbojet engine is modelled with the pseudo bond graph approach in this paper. This theory is implemented in the in-house software tool ASTOR (AircraftEngine Simulation of Transient Operation Research) to simulate the overall dynamic of the turbojet model engine P200SX. In ASTOR, the transient performance is calculated with dynamic and individual control volumes to determine the three conservation equations. In this investigation a stationary operating point and a transient load case are simulated and compared to results of a commercial software and a measurement.
KW - Bond graph theory
KW - Gas turbine
KW - Jet engine
UR - http://www.scopus.com/inward/record.url?scp=85073152972&partnerID=8YFLogxK
U2 - 10.1007/978-3-030-25253-3_41
DO - 10.1007/978-3-030-25253-3_41
M3 - Contribution to book/anthology
SN - 978-3-030-25252-6
SN - 978-3-030-25255-7
T3 - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
SP - 427
EP - 436
BT - New Results in Numerical and Experimental Fluid Mechanics XII
A2 - Dillmann, Andreas
A2 - Heller, Gerd
A2 - Krämer, Ewald
A2 - Wagner, Claus
A2 - Tropea, Cameron
A2 - Jakirlić, Suad
T2 - Symposium der Deutsche Gesellschaft für Luft- und Raumfahrt
Y2 - 6 November 2018 through 7 November 2018
ER -